Squash history after removing .frd solver outputs

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/_gmsh_run.py

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+import gmsh, sys
+gmsh.initialize()
+gmsh.option.setNumber("General.Terminal", 1)
+gmsh.option.setNumber("Mesh.Algorithm3D", 10)   # HXT for tets
+gmsh.option.setNumber("Mesh.MeshSizeFromCurvature", 12)
+gmsh.option.setNumber("Mesh.MeshSizeMin", 1.0)
+gmsh.option.setNumber("Mesh.MeshSizeMax", 50.0)
+# Only export elements in physical groups (skips edge T3D2 / face CPS3 noise that
+# breaks *SOLID SECTION).
+gmsh.option.setNumber("Mesh.SaveAll", 0)
+# Emit named *ELSETs from physical groups (one per group).
+gmsh.option.setNumber("Mesh.SaveGroupsOfElements", 1)
+gmsh.open('/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/out.step')
+gmsh.model.occ.synchronize()
+vols = [tag for (dim, tag) in gmsh.model.getEntities(3)]
+if not vols:
+    sys.exit("ERROR: STEP file contains no 3D volumes")
+
+body_elsets = []
+if body_elsets and len(body_elsets) == len(vols):
+    # Multi-material conformal meshing: fragment the volumes so
+    # coincident faces (e.g. a liner-wrap bonded interface) become
+    # shared topology with shared mesh nodes. fragment returns a list
+    # of tag-pairs in the SAME ORDER as the input vols, so we can map
+    # each result volume back to its body name.
+    in_dimtags = [(3, v) for v in vols]
+    out_dimtags, out_map = gmsh.model.occ.fragment(in_dimtags, [])
+    gmsh.model.occ.synchronize()
+    # out_map[i] is the list of dim-tags that resulted from input i.
+    # For two non-overlapping volumes that share a face, each input
+    # maps to exactly one output volume (the face is now shared).
+    # Group volumes by ELSET name first so that multiple bodies sharing
+    # a name (e.g. four corner rails all tagged "RAIL") end up in one
+    # physical group / one *ELSET in the meshed .inp.
+    name_to_vols = {}
+    for i, name in enumerate(body_elsets):
+        new_vols = [tag for (dim, tag) in out_map[i] if dim == 3]
+        if not new_vols:
+            sys.exit(f"ERROR: fragment lost body '{name}' (input volume {vols[i]})")
+        name_to_vols.setdefault(name, []).extend(new_vols)
+    for name, group_vols in name_to_vols.items():
+        gmsh.model.addPhysicalGroup(3, group_vols, name=name)
+else:
+    # Single-material legacy: one group "VOLUME" for all volumes.
+    gmsh.model.addPhysicalGroup(3, vols, name="VOLUME")
+
+gmsh.model.mesh.generate(3)
+gmsh.write('/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/mesh.inp')
+gmsh.finalize()

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/analysis_template.inp

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+**
+** Generic CCX multipart coverage deck for 033_s2_ecss_32_10c_spacecraft_panel
+** Generated by scripts/ccx_eval/generate_multipart_coverage_kits.py
+** Units: mm, N, MPa, tonne, s
+**
+*MATERIAL, NAME=__MATERIAL__
+*ELASTIC
+70000.0, 0.33
+*DENSITY
+2.70e-9
+*CONDUCTIVITY
+167.0
+*SPECIFIC HEAT
+8.96e8
+*EXPANSION
+2.30e-5
+**
+*SOLID SECTION, ELSET=Eall, MATERIAL=__MATERIAL__
+**
+*BOUNDARY
+NFIXED, 1, 3, 0.0
+*INITIAL CONDITIONS, TYPE=TEMPERATURE
+NALL, 293.0
+
+**
+** STEP 1: generated static coverage for LC1
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 2, -100
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 2: generated static coverage for LC2
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 3, -80
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 3: generated static coverage for LC3
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 1, 60
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 4: generated static coverage for LC4
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 2, 45
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** Modal coverage
+*STEP
+*FREQUENCY, STORAGE=YES
+6
+*END STEP
+
+**
+** Buckling coverage
+*STEP
+*BUCKLE
+4
+*CLOAD
+NLOAD, 2, -1.0
+*END STEP

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/build.py

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+"""ECSS-E-ST-32-10C spacecraft equipment panel: aluminum-honeycomb sandwich.
+
+Builds a multi-part assembly (face sheets + core + edge frames + 8 equipment
+masses), fuses to a single solid for STEP export, and writes meta.json
+following the FEA eval contract.
+
+Coordinate convention:
+    X: along 1200 mm long edge
+    Y: along 800 mm short edge
+    Z: through-thickness (z=0 at bottom face sheet exterior, z=25.4 at top face)
+"""
+from __future__ import annotations
+
+import json
+import math
+from pathlib import Path
+
+import cadquery as cq
+
+# ---------- Dimensions (mm) ----------
+PANEL_L = 1200.0
+PANEL_W = 800.0
+PANEL_T = 25.4
+
+FACESHEET_T = 0.5
+CORE_T = PANEL_T - 2.0 * FACESHEET_T  # 24.4
+
+FRAME_W = 25.0          # frame in-plane width
+FRAME_H = PANEL_T       # frame full panel height
+
+EQ_L = 100.0
+EQ_W = 80.0
+EQ_H = 40.0
+EQ_NX = 4
+EQ_NY = 2
+EQ_MASS_KG = 3.0
+
+# Material (AA 2024-T3)
+MATERIAL_NAME = "AA_2024_T3"
+E_MPA = 73100.0
+NU = 0.33
+RHO_KG_M3 = 2780.0
+
+
+def _box(L: float, W: float, H: float, cx: float, cy: float, cz: float) -> cq.Workplane:
+    """Create a box centered at (cx,cy,cz)."""
+    return (
+        cq.Workplane("XY")
+        .box(L, W, H, centered=(True, True, True))
+        .translate((cx, cy, cz))
+    )
+
+
+def build_assembly() -> cq.Workplane:
+    parts: list[cq.Workplane] = []
+
+    # Bottom face sheet: 1200 x 800 x 0.5, centered at z = 0.25
+    bottom = _box(PANEL_L, PANEL_W, FACESHEET_T,
+                  PANEL_L / 2.0, PANEL_W / 2.0, FACESHEET_T / 2.0)
+    parts.append(bottom)
+
+    # Honeycomb core: 1200 x 800 x 24.4, centered at z = 0.5 + 12.2 = 12.7
+    core = _box(PANEL_L, PANEL_W, CORE_T,
+                PANEL_L / 2.0, PANEL_W / 2.0, FACESHEET_T + CORE_T / 2.0)
+    parts.append(core)
+
+    # Top face sheet: centered at z = 25.15
+    top = _box(PANEL_L, PANEL_W, FACESHEET_T,
+               PANEL_L / 2.0, PANEL_W / 2.0, PANEL_T - FACESHEET_T / 2.0)
+    parts.append(top)
+
+    # Edge close-out frames (4 sides, full panel height)
+    # Note: frames overlap the face sheets/core volumetrically; the union fuses
+    # them into one solid which is fine for STEP export and meshing.
+    # x_min frame: 25 wide x 800 long x 25.4 tall, centered at x=12.5, y=400, z=12.7
+    frame_xmin = _box(FRAME_W, PANEL_W, FRAME_H,
+                      FRAME_W / 2.0, PANEL_W / 2.0, FRAME_H / 2.0)
+    parts.append(frame_xmin)
+
+    frame_xmax = _box(FRAME_W, PANEL_W, FRAME_H,
+                      PANEL_L - FRAME_W / 2.0, PANEL_W / 2.0, FRAME_H / 2.0)
+    parts.append(frame_xmax)
+
+    # y_min and y_max frames span only between the x frames to avoid corner overlap nesting
+    frame_y_len = PANEL_L - 2.0 * FRAME_W
+    frame_ymin = _box(frame_y_len, FRAME_W, FRAME_H,
+                      PANEL_L / 2.0, FRAME_W / 2.0, FRAME_H / 2.0)
+    parts.append(frame_ymin)
+
+    frame_ymax = _box(frame_y_len, FRAME_W, FRAME_H,
+                      PANEL_L / 2.0, PANEL_W - FRAME_W / 2.0, FRAME_H / 2.0)
+    parts.append(frame_ymax)
+
+    # Equipment masses (4 x 2 grid on top face sheet upper surface)
+    eq_centers: list[tuple[float, float, float]] = []
+    pitch_x = PANEL_L / (EQ_NX + 1)  # 240 mm
+    pitch_y = PANEL_W / (EQ_NY + 1)  # ~266.67 mm
+    for ix in range(EQ_NX):
+        for iy in range(EQ_NY):
+            cx = pitch_x * (ix + 1) + (PANEL_L - pitch_x * (EQ_NX + 1)) / 2.0
+            # Use simple even spacing: column centers at pitch_x*(ix+1)
+            cx = pitch_x * (ix + 1)
+            cy = pitch_y * (iy + 1)
+            cz = PANEL_T + EQ_H / 2.0
+            eq_centers.append((cx, cy, cz))
+            parts.append(_box(EQ_L, EQ_W, EQ_H, cx, cy, cz))
+
+    # Fuse everything into a single compound solid for STEP export
+    result = parts[0]
+    for p in parts[1:]:
+        result = result.union(p)
+
+    return result, eq_centers
+
+
+def panel_mass_kg() -> float:
+    """Approx panel mass (face sheets + core + frames + 8 equipment blocks)."""
+    rho_face = 2780.0  # AA 2024-T3 kg/m^3
+    rho_core = 50.0    # Al 5056 honeycomb kg/m^3
+    # Convert mm^3 -> m^3
+    mm3_to_m3 = 1.0e-9
+    v_face = 2.0 * (PANEL_L * PANEL_W * FACESHEET_T) * mm3_to_m3
+    v_core = (PANEL_L * PANEL_W * CORE_T) * mm3_to_m3
+    v_frame = (
+        2.0 * (FRAME_W * PANEL_W * FRAME_H)
+        + 2.0 * ((PANEL_L - 2.0 * FRAME_W) * FRAME_W * FRAME_H)
+    ) * mm3_to_m3
+    m_eq = EQ_NX * EQ_NY * EQ_MASS_KG
+    return rho_face * v_face + rho_core * v_core + rho_face * v_frame + m_eq
+
+
+def main() -> None:
+    out_dir = Path(__file__).parent
+    step_path = out_dir / "out.step"
+    meta_path = out_dir / "meta.json"
+
+    solid, eq_centers = build_assembly()
+
+    # Export STEP (AP242 / AP214)
+    cq.exporters.export(solid, str(step_path), exportType="STEP")
+
+    # Engineering metrics from chosen geometry
+    panel_mass = panel_mass_kg()
+    total_eq_mass = EQ_NX * EQ_NY * EQ_MASS_KG
+
+    meta = {
+        "jobname": "model",
+        "material": MATERIAL_NAME,
+        "material_props": {
+            "E_MPa": E_MPA,
+            "nu": NU,
+            "density_kg_m3": RHO_KG_M3,
+        },
+        "selectors": {
+            "NFIXED": {"face": "z_min", "tol_mm": 0.5},
+            "NALL": {"all": True},
+            "NLOAD": {"face_eq": "z", "value": PANEL_T, "tol_mm": 0.5},
+        },
+        "engineering_metrics": {
+            "panel_length_mm": PANEL_L,
+            "panel_width_mm": PANEL_W,
+            "panel_thickness_mm": PANEL_T,
+            "face_sheet_thickness_mm": FACESHEET_T,
+            "core_thickness_mm": CORE_T,
+            "edge_frame_width_mm": FRAME_W,
+            "edge_frame_height_mm": FRAME_H,
+            "equipment_count": EQ_NX * EQ_NY,
+            "equipment_mass_kg_each": EQ_MASS_KG,
+            "total_equipment_mass_kg": total_eq_mass,
+            "panel_mass_kg_estimate": round(panel_mass, 4),
+            "first_mode_Hz_target": 80.0,
+            "lc1_axial_g": 12.5,
+            "lc1_lateral_g": 8.0,
+            "lc2_miles_g": 20.0,
+            "lc3_dT_top_C": 80.0,
+            "lc3_dT_bottom_C": -100.0,
+            "lc4_edge_load_N_per_m": 4000.0,
+            "ecss_KY": 1.25,
+            "ecss_KU": 1.25,
+            "ecss_KM": 1.0,
+        },
+        "equipment_centers_mm": [list(c) for c in eq_centers],
+        "load_cases": {
+            "LC1_quasi_static_launch": {
+                "type": "quasi_static",
+                "axial_g": 12.5,
+                "lateral_g": 8.0,
+                "applied_at": "equipment_mass_centers",
+            },
+            "LC2_random_miles_equivalent": {
+                "type": "miles_equivalent",
+                "out_of_plane_g": 20.0,
+                "first_mode_Hz": 80.0,
+                "psd_g2_per_Hz": 0.2,
+            },
+            "LC3_thermoelastic": {
+                "type": "thermal_gradient",
+                "dT_top_C": 80.0,
+                "dT_bottom_C": -100.0,
+            },
+            "LC4_inplane_compression": {
+                "type": "edge_load",
+                "value_N_per_m": 4000.0,
+                "edges": ["x_min", "x_max"],
+            },
+        },
+    }
+
+    with open(meta_path, "w") as f:
+        json.dump(meta, f, indent=2)
+
+    # Sanity check
+    size = step_path.stat().st_size
+    print(f"Wrote {step_path} ({size} bytes)")
+    print(f"Wrote {meta_path}")
+
+
+if __name__ == "__main__":
+    main()

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/check.log

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+[PASS] R1 class=FEA_STRUCTURAL source=experiment=EXP_R1_000 card=*STATIC step=generated_static_step:LC1,LC2,LC3 source=static stress/displacement block
+[PASS] R2 class=FEA_STRUCTURAL source=experiment=EXP_R2_001 card=*STATIC step=generated_static_step:LC1,LC2,LC3 source=static stress/displacement block
+[PASS] R3 class=FEA_STRUCTURAL source=experiment=EXP_R3_002 card=*STATIC step=generated_static_step:LC1,LC2 source=static stress/displacement block
+[PASS] R4 class=FEA_BUCKLING source=experiment=EXP_R4_003 card=*BUCKLE step=generated_buckling_step source=buckling eigenvalue block
+[PASS] R5 class=FEA_MODAL source=experiment=EXP_R5_004 card=*FREQUENCY step=generated_modal_step source=modal eigenfrequency block
+[PASS] R6 class=GEOMETRIC source=experiment=EXP_R6_005 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+[PASS] R_GEOMETRY_COVERAGE class=GEOMETRIC source=experiment=EXP_R_GEOMETRY_COVERAGE_006 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+SUMMARY PASS=7 FAIL=0 SKIP=0 TOTAL=7

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/check.py

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+#!/usr/bin/env python3
+"""Generated CCX coverage checker for 033_s2_ecss_32_10c_spacecraft_panel.
+
+Generated by scripts/ccx_eval/generate_multipart_coverage_kits.py
+"""
+from __future__ import annotations
+
+import json
+import math
+import re
+import sys
+from pathlib import Path
+
+
+HERE = Path(__file__).resolve().parent
+SPEC = HERE / "spec.json"
+DAT = HERE / "model.dat"
+
+
+def walk_text(value):
+    parts = []
+    def walk(v):
+        if isinstance(v, dict):
+            for k, item in v.items():
+                parts.append(str(k)); walk(item)
+        elif isinstance(v, list):
+            for item in v:
+                walk(item)
+        elif v is not None:
+            parts.append(str(v))
+    walk(value)
+    return " ".join(parts).lower()
+
+
+def classify(req):
+    text = walk_text(req)
+    rtype = str(req.get("type") or "").lower()
+    metric = str(req.get("metric") or "").lower()
+    if "buckl" in text:
+        return "FEA_BUCKLING"
+    if any(k in text for k in ("natural_frequency", "modal", "mode_hz", "frequency")):
+        return "FEA_MODAL"
+    if any(k in text for k in ("thermal", "temperature", "heat")):
+        return "FEA_THERMAL"
+    if any(k in text for k in ("contact pressure", "contact_pressure", "gap opening", "gap status", "gap_opening")):
+        return "FEA_CONTACT"
+    if any(k in text for k in ("fatigue", "random", "vibration", "shock", "srs", "dynamic", "sine", "miner")):
+        return "FEA_OTHER"
+    response = ("stress", "strain", "deflection", "displacement", "drift", "sway", "dcr", "shear",
+                "von_mises", "tsai", "failure_index", "load_factor", "pressure", "preload",
+                "slip", "growth", "ovalization")
+    geom = ("mass", "weight", "density", "dry_mass", "wet_mass", "self_weight", "envelope",
+            "bounding_box", "count", "width", "length", "diameter", "straightness", "volume",
+            "height", "wall_thickness", "geometry", "geometric")
+    if any(k in metric for k in geom) or any(k in rtype for k in ("geometric", "dimensional")):
+        return "GEOMETRIC"
+    if any(k in text for k in response):
+        return "FEA_STRUCTURAL"
+    if rtype in {"structural_analysis", "assembly_analysis", "connection_integrity",
+                 "connection_check", "code_check", "assembled_model"}:
+        return "FEA_STRUCTURAL"
+    return "GEOMETRIC"
+
+
+def dat_features():
+    if not DAT.exists():
+        return {"has_dat": False}
+    text = DAT.read_text(errors="ignore").lower()
+    return {
+        "has_dat": True,
+        "static": ("stresses" in text) or ("displacements" in text),
+        "modal": ("eigenfrequency" in text) or ("eigenvalue output" in text) or ("frequency" in text),
+        "buckling": ("buckling" in text) or ("eigenvalue" in text),
+        "thermal": ("temperatures" in text) or ("temperature" in text),
+        "dynamic": ("displacements" in text) or ("stresses" in text),
+        "contact": ("displacements" in text) or ("contact" in text),
+    }
+
+
+def requirement_covered(cls, features):
+    if cls == "GEOMETRIC":
+        return True, "geometry/spec assertion"
+    if not features.get("has_dat"):
+        return False, "model.dat missing"
+    if cls == "FEA_MODAL":
+        return bool(features.get("modal")), "modal eigenfrequency block"
+    if cls == "FEA_BUCKLING":
+        return bool(features.get("buckling")), "buckling eigenvalue block"
+    if cls == "FEA_THERMAL":
+        return bool(features.get("thermal")), "thermal temperature block"
+    if cls == "FEA_OTHER":
+        return bool(features.get("dynamic")), "dynamic/static response block"
+    if cls == "FEA_CONTACT":
+        return bool(features.get("contact")), "contact/gap displacement response"
+    return bool(features.get("static")), "static stress/displacement block"
+
+
+def experiment_covered(experiment, features):
+    cls = str(experiment.get("requirement_class") or "")
+    solver = str(experiment.get("solver") or "")
+    if solver == "geometry" or cls == "GEOMETRIC":
+        return True, "geometry/spec assertion"
+    if not features.get("has_dat"):
+        return False, "model.dat missing"
+    return requirement_covered(cls, features)
+
+
+def main():
+    spec = json.loads(SPEC.read_text())
+    reqs = (spec.get("requirements") or {}).get("pass_fail_criteria") or []
+    experiments = spec.get("fea_experiments") or []
+    features = dat_features()
+    rows = []
+    req_ids = [str(req.get("id") or f"REQ_{i}") for i, req in enumerate(reqs)]
+    experiment_req_ids = [str(exp.get("requirement_id") or "") for exp in experiments]
+    for rid in req_ids:
+        if rid not in experiment_req_ids:
+            rows.append((rid, "NO_EXPERIMENT", "FAIL", "missing fea_experiments entry"))
+    for experiment in experiments:
+        rid = str(experiment.get("requirement_id") or experiment.get("id") or "UNKNOWN")
+        cls = str(experiment.get("requirement_class") or "UNKNOWN")
+        ok, source = experiment_covered(experiment, features)
+        card = experiment.get("analysis_card")
+        step = experiment.get("deck_step")
+        rows.append((rid, cls, "PASS" if ok else "FAIL", f"experiment={experiment.get('id')} card={card} step={step} source={source}"))
+
+    for rid, cls, verdict, source in rows:
+        print(f"[{verdict}] {rid} class={cls} source={source}")
+
+    n_pass = sum(1 for _, _, verdict, _ in rows if verdict == "PASS")
+    n_fail = sum(1 for _, _, verdict, _ in rows if verdict == "FAIL")
+    print(f"SUMMARY PASS={n_pass} FAIL={n_fail} SKIP=0 TOTAL={len(rows)}")
+    return 0 if n_fail == 0 else 2
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/engineering_check.log

@@ -0,0 +1,7 @@
+[PASS] R1 class=ENGINEERING source=metric=max_static_von_mises_MPa value=0.408729 requirement=<= 232 source=generic_multi_engineering_checker
+[PASS] R2 class=ENGINEERING source=metric=max_static_von_mises_MPa value=0.408729 requirement=<= 348 source=generic_multi_engineering_checker
+[PASS] R3 class=ENGINEERING source=metric=max_static_shear_MPa value=0.164781 requirement=<= 1.54 source=generic_multi_engineering_checker
+[PASS] R4 class=ENGINEERING source=metric=min_buckling_factor value=3.75685e+07 requirement=>= 1.25 source=generic_multi_engineering_checker
+[PASS] R5 class=ENGINEERING source=metric=min_modal_frequency_Hz value=15276.1 requirement=>= 70 source=generic_multi_engineering_checker
+[FAIL] R6 class=ENGINEERING source=missing mesh mass or planform area for areal density
+SUMMARY PASS=5 FAIL=1 SKIP=0 TOTAL=6

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/eval_driver.log

@@ -0,0 +1,11 @@
+--- check.log ---
+[PASS] R1 class=FEA_STRUCTURAL source=experiment=EXP_R1_000 card=*STATIC step=generated_static_step:LC1,LC2,LC3 source=static stress/displacement block
+[PASS] R2 class=FEA_STRUCTURAL source=experiment=EXP_R2_001 card=*STATIC step=generated_static_step:LC1,LC2,LC3 source=static stress/displacement block
+[PASS] R3 class=FEA_STRUCTURAL source=experiment=EXP_R3_002 card=*STATIC step=generated_static_step:LC1,LC2 source=static stress/displacement block
+[PASS] R4 class=FEA_BUCKLING source=experiment=EXP_R4_003 card=*BUCKLE step=generated_buckling_step source=buckling eigenvalue block
+[PASS] R5 class=FEA_MODAL source=experiment=EXP_R5_004 card=*FREQUENCY step=generated_modal_step source=modal eigenfrequency block
+[PASS] R6 class=GEOMETRIC source=experiment=EXP_R6_005 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+[PASS] R_GEOMETRY_COVERAGE class=GEOMETRIC source=experiment=EXP_R_GEOMETRY_COVERAGE_006 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+SUMMARY PASS=7 FAIL=0 SKIP=0 TOTAL=7
+
+=== final rc=0: check.py rc=0

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/grade.json

@@ -0,0 +1,27 @@
+{
+  "workdir": "/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel",
+  "stages": {
+    "build": {
+      "rc": 0,
+      "elapsed_s": 0.98
+    },
+    "gmsh": {
+      "rc": 0,
+      "elapsed_s": 0.2
+    },
+    "wire_bcs": {
+      "rc": 0,
+      "elapsed_s": 0.02
+    },
+    "ccx": {
+      "rc": 0,
+      "elapsed_s": 0.4
+    },
+    "check": {
+      "rc": 0,
+      "elapsed_s": 0.04
+    }
+  },
+  "final_rc": 0,
+  "final_msg": "check.py rc=0"
+}

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/grade.log

@@ -0,0 +1,479 @@
+# grade_ccx run @ 2026-05-04 13:28:46
+# workdir: /Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel
+
+$ /opt/anaconda3/envs/cadquery/bin/python build.py
+Wrote /Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/out.step (132347 bytes)
+Wrote /Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/meta.json
+
+[rc=0]
+
+$ /opt/anaconda3/envs/cadquery/bin/python /Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/_gmsh_run.py
+Info    : Reading '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/out.step'...
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1' (3D)
+Info    : Done reading '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/out.step'
+Info    : Meshing 1D...
+Info    : [  0%] Meshing curve 1 (Line)
+Info    : [ 10%] Meshing curve 2 (Line)
+Info    : [ 10%] Meshing curve 3 (Line)
+Info    : [ 10%] Meshing curve 4 (Line)
+Info    : [ 10%] Meshing curve 5 (Line)
+Info    : [ 10%] Meshing curve 6 (Line)
+Info    : [ 10%] Meshing curve 7 (Line)
+Info    : [ 10%] Meshing curve 8 (Line)
+Info    : [ 10%] Meshing curve 9 (Line)
+Info    : [ 10%] Meshing curve 10 (Line)
+Info    : [ 10%] Meshing curve 11 (Line)
+Info    : [ 20%] Meshing curve 12 (Line)
+Info    : [ 20%] Meshing curve 13 (Line)
+Info    : [ 20%] Meshing curve 14 (Line)
+Info    : [ 20%] Meshing curve 15 (Line)
+Info    : [ 20%] Meshing curve 16 (Line)
+Info    : [ 20%] Meshing curve 17 (Line)
+Info    : [ 20%] Meshing curve 18 (Line)
+Info    : [ 20%] Meshing curve 19 (Line)
+Info    : [ 20%] Meshing curve 20 (Line)
+Info    : [ 20%] Meshing curve 21 (Line)
+Info    : [ 20%] Meshing curve 22 (Line)
+Info    : [ 30%] Meshing curve 23 (Line)
+Info    : [ 30%] Meshing curve 24 (Line)
+Info    : [ 30%] Meshing curve 25 (Line)
+Info    : [ 30%] Meshing curve 26 (Line)
+Info    : [ 30%] Meshing curve 27 (Line)
+Info    : [ 30%] Meshing curve 28 (Line)
+Info    : [ 30%] Meshing curve 29 (Line)
+Info    : [ 30%] Meshing curve 30 (Line)
+Info    : [ 30%] Meshing curve 31 (Line)
+Info    : [ 30%] Meshing curve 32 (Line)
+Info    : [ 30%] Meshing curve 33 (Line)
+Info    : [ 40%] Meshing curve 34 (Line)
+Info    : [ 40%] Meshing curve 35 (Line)
+Info    : [ 40%] Meshing curve 36 (Line)
+Info    : [ 40%] Meshing curve 37 (Line)
+Info    : [ 40%] Meshing curve 38 (Line)
+Info    : [ 40%] Meshing curve 39 (Line)
+Info    : [ 40%] Meshing curve 40 (Line)
+Info    : [ 40%] Meshing curve 41 (Line)
+Info    : [ 40%] Meshing curve 42 (Line)
+Info    : [ 40%] Meshing curve 43 (Line)
+Info    : [ 40%] Meshing curve 44 (Line)
+Info    : [ 50%] Meshing curve 45 (Line)
+Info    : [ 50%] Meshing curve 46 (Line)
+Info    : [ 50%] Meshing curve 47 (Line)
+Info    : [ 50%] Meshing curve 48 (Line)
+Info    : [ 50%] Meshing curve 49 (Line)
+Info    : [ 50%] Meshing curve 50 (Line)
+Info    : [ 50%] Meshing curve 51 (Line)
+Info    : [ 50%] Meshing curve 52 (Line)
+Info    : [ 50%] Meshing curve 53 (Line)
+Info    : [ 50%] Meshing curve 54 (Line)
+Info    : [ 60%] Meshing curve 55 (Line)
+Info    : [ 60%] Meshing curve 56 (Line)
+Info    : [ 60%] Meshing curve 57 (Line)
+Info    : [ 60%] Meshing curve 58 (Line)
+Info    : [ 60%] Meshing curve 59 (Line)
+Info    : [ 60%] Meshing curve 60 (Line)
+Info    : [ 60%] Meshing curve 61 (Line)
+Info    : [ 60%] Meshing curve 62 (Line)
+Info    : [ 60%] Meshing curve 63 (Line)
+Info    : [ 60%] Meshing curve 64 (Line)
+Info    : [ 60%] Meshing curve 65 (Line)
+Info    : [ 70%] Meshing curve 66 (Line)
+Info    : [ 70%] Meshing curve 67 (Line)
+Info    : [ 70%] Meshing curve 68 (Line)
+Info    : [ 70%] Meshing curve 69 (Line)
+Info    : [ 70%] Meshing curve 70 (Line)
+Info    : [ 70%] Meshing curve 71 (Line)
+Info    : [ 70%] Meshing curve 72 (Line)
+Info    : [ 70%] Meshing curve 73 (Line)
+Info    : [ 70%] Meshing curve 74 (Line)
+Info    : [ 70%] Meshing curve 75 (Line)
+Info    : [ 70%] Meshing curve 76 (Line)
+Info    : [ 80%] Meshing curve 77 (Line)
+Info    : [ 80%] Meshing curve 78 (Line)
+Info    : [ 80%] Meshing curve 79 (Line)
+Info    : [ 80%] Meshing curve 80 (Line)
+Info    : [ 80%] Meshing curve 81 (Line)
+Info    : [ 80%] Meshing curve 82 (Line)
+Info    : [ 80%] Meshing curve 83 (Line)
+Info    : [ 80%] Meshing curve 84 (Line)
+Info    : [ 80%] Meshing curve 85 (Line)
+Info    : [ 80%] Meshing curve 86 (Line)
+Info    : [ 80%] Meshing curve 87 (Line)
+Info    : [ 90%] Meshing curve 88 (Line)
+Info    : [ 90%] Meshing curve 89 (Line)
+Info    : [ 90%] Meshing curve 90 (Line)
+Info    : [ 90%] Meshing curve 91 (Line)
+Info    : [ 90%] Meshing curve 92 (Line)
+Info    : [ 90%] Meshing curve 93 (Line)
+Info    : [ 90%] Meshing curve 94 (Line)
+Info    : [ 90%] Meshing curve 95 (Line)
+Info    : [ 90%] Meshing curve 96 (Line)
+Info    : [ 90%] Meshing curve 97 (Line)
+Info    : [ 90%] Meshing curve 98 (Line)
+Info    : [100%] Meshing curve 99 (Line)
+Info    : [100%] Meshing curve 100 (Line)
+Info    : [100%] Meshing curve 101 (Line)
+Info    : [100%] Meshing curve 102 (Line)
+Info    : [100%] Meshing curve 103 (Line)
+Info    : [100%] Meshing curve 104 (Line)
+Info    : [100%] Meshing curve 105 (Line)
+Info    : [100%] Meshing curve 106 (Line)
+Info    : [100%] Meshing curve 107 (Line)
+Info    : [100%] Meshing curve 108 (Line)
+Info    : Done meshing 1D (Wall 0.0302127s, CPU 0.029915s)
+Info    : Meshing 2D...
+Info    : [  0%] Meshing surface 1 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 2 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 3 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 4 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 5 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 6 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 7 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 8 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 9 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 10 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 11 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 12 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 13 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 14 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 15 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 16 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 17 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 18 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 19 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 20 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 21 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 22 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 23 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 24 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 25 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 26 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 27 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 28 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 29 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 30 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 31 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 32 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 33 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 34 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 35 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 36 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 37 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 38 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 39 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 40 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 41 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 42 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 43 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 44 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 45 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 46 (Plane, Frontal-Delaunay)
+Info    : Done meshing 2D (Wall 0.0542314s, CPU 0.053848s)
+Info    : Meshing 3D...
+Info    : 3D Meshing 1 volume with 1 connected component
+Info    : Input mesh hash f37548f45f26fc0d
+Info    : Creating an empty mesh with 1343 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of       1339 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 32 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving        119 tet. on   1 thrd (S & ER)
+Info    : Improving          8 tet. on   1 thrd (S & ER)
+Info    : Improving          3 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 7010 tetrahedra
+Info    :  	Final tet. mesh contains 1343 vertices
+Info    : tEmptyMesh  	 = 	    0.004
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.003
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Done meshing 3D (Wall 0.00982042s, CPU 0.009331s)
+Info    : 1343 nodes 6920 elements
+Info    : Writing '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/mesh.inp'...
+Info    : Done writing '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/mesh.inp'
+
+[rc=0]
+
+$ /opt/anaconda3/envs/cadquery/bin/python /Users/songuijin/Documents/GitHub/Hephaestus/scripts/ccx_eval/wire_bcs.py mesh.inp meta.json analysis_template.inp model.inp
+  NSET=NFIXED: 495 nodes
+  NSET=NALL: 1343 nodes
+  NSET=NLOAD: 616 nodes
+wrote model.inp: 1343 nodes, NSETs=['NFIXED', 'NALL', 'NLOAD'], Eall = ['Volume1']
+
+[rc=0]
+
+$ /opt/homebrew/bin/ccx_2.22 model
+
+************************************************************
+
+CalculiX Version 2.22, Copyright(C) 1998-2024 Guido Dhondt
+CalculiX comes with ABSOLUTELY NO WARRANTY. This is free
+software, and you are welcome to redistribute it under
+certain conditions, see gpl.htm
+
+************************************************************
+
+You are using an executable made on Wed Feb 11 07:16:28 UTC 2026
+ Decascading the MPC's
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 2544
+ number of nonzero lower triangular matrix elements
+ 26700
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 2544
+ number of nonzero lower triangular matrix elements
+ 26700
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 2544
+ number of nonzero lower triangular matrix elements
+ 26700
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 2544
+ number of nonzero lower triangular matrix elements
+ 26700
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 2544
+ number of nonzero lower triangular matrix elements
+ 26700
+
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Calculating the eigenvalues and the eigenmodes
+
+U^T*M*U=1.000002 for eigenmode 1
+U^T*M*U=1.000030 for eigenmode 2
+sum=1.000030e+00
+normalizing the eigenmode 
+U^T*M*U=1.000052 for eigenmode 3
+sum=1.000052e+00
+normalizing the eigenmode 
+U^T*M*U=1.000035 for eigenmode 4
+sum=1.000035e+00
+normalizing the eigenmode 
+U^T*M*U=1.000073 for eigenmode 5
+sum=1.000073e+00
+normalizing the eigenmode 
+U^T*M*U=1.000052 for eigenmode 6
+sum=1.000052e+00
+normalizing the eigenmode 
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 2544
+ number of nonzero lower triangular matrix elements
+ 26700
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Calculating the buckling factors and buckling modes:
+
+sigma=1.000000,d[0]=37568473.332623
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+________________________________________
+
+Total CalculiX Time: 0.341894
+________________________________________
+
+  The numbers below are estimated upper bounds
+
+  number of:
+
+   nodes:         1343
+   elements:         3842
+   one-dimensional elements:            0
+   two-dimensional elements:            0
+   integration points per element:            1
+   degrees of freedom per node:            3
+   layers per element:            1
+
+   distributed facial loads:            0
+   distributed volumetric loads:            0
+   concentrated loads:         3080
+   single point constraints:         1485
+   multiple point constraints:            1
+   terms in all multiple point constraints:            1
+   tie constraints:            0
+   dependent nodes tied by cyclic constraints:            0
+   dependent nodes in pre-tension constraints:            0
+
+   sets:            6
+   terms in all sets:        17822
+
+   materials:            1
+   constants per material and temperature:            2
+   temperature points per material:            1
+   plastic data points per material:            0
+
+   orientations:            0
+   amplitudes:            6
+   data points in all amplitudes:            6
+   print requests:            8
+   transformations:            0
+   property cards:            0
+
+
+ STEP            1
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+
+ STEP            2
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+
+ STEP            3
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+
+ STEP            4
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+
+ STEP            5
+
+ Frequency analysis was selected
+
+
+ STEP            6
+
+ Buckling analysis was selected
+
+
+ Job finished
+
+
+[rc=0]

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/meta.json

@@ -0,0 +1,115 @@
+{
+  "jobname": "model",
+  "material": "AA_2024_T3",
+  "material_props": {
+    "E_MPa": 73100.0,
+    "nu": 0.33,
+    "density_kg_m3": 2780.0
+  },
+  "selectors": {
+    "NFIXED": {
+      "face": "z_min",
+      "tol_mm": 0.5
+    },
+    "NALL": {
+      "all": true
+    },
+    "NLOAD": {
+      "face_eq": "z",
+      "value": 25.4,
+      "tol_mm": 0.5
+    }
+  },
+  "engineering_metrics": {
+    "panel_length_mm": 1200.0,
+    "panel_width_mm": 800.0,
+    "panel_thickness_mm": 25.4,
+    "face_sheet_thickness_mm": 0.5,
+    "core_thickness_mm": 24.4,
+    "edge_frame_width_mm": 25.0,
+    "edge_frame_height_mm": 25.4,
+    "equipment_count": 8,
+    "equipment_mass_kg_each": 3.0,
+    "total_equipment_mass_kg": 24.0,
+    "panel_mass_kg_estimate": 34.7247,
+    "first_mode_Hz_target": 80.0,
+    "lc1_axial_g": 12.5,
+    "lc1_lateral_g": 8.0,
+    "lc2_miles_g": 20.0,
+    "lc3_dT_top_C": 80.0,
+    "lc3_dT_bottom_C": -100.0,
+    "lc4_edge_load_N_per_m": 4000.0,
+    "ecss_KY": 1.25,
+    "ecss_KU": 1.25,
+    "ecss_KM": 1.0
+  },
+  "equipment_centers_mm": [
+    [
+      240.0,
+      266.6666666666667,
+      45.4
+    ],
+    [
+      240.0,
+      533.3333333333334,
+      45.4
+    ],
+    [
+      480.0,
+      266.6666666666667,
+      45.4
+    ],
+    [
+      480.0,
+      533.3333333333334,
+      45.4
+    ],
+    [
+      720.0,
+      266.6666666666667,
+      45.4
+    ],
+    [
+      720.0,
+      533.3333333333334,
+      45.4
+    ],
+    [
+      960.0,
+      266.6666666666667,
+      45.4
+    ],
+    [
+      960.0,
+      533.3333333333334,
+      45.4
+    ]
+  ],
+  "load_cases": {
+    "LC1_quasi_static_launch": {
+      "type": "quasi_static",
+      "axial_g": 12.5,
+      "lateral_g": 8.0,
+      "applied_at": "equipment_mass_centers"
+    },
+    "LC2_random_miles_equivalent": {
+      "type": "miles_equivalent",
+      "out_of_plane_g": 20.0,
+      "first_mode_Hz": 80.0,
+      "psd_g2_per_Hz": 0.2
+    },
+    "LC3_thermoelastic": {
+      "type": "thermal_gradient",
+      "dT_top_C": 80.0,
+      "dT_bottom_C": -100.0
+    },
+    "LC4_inplane_compression": {
+      "type": "edge_load",
+      "value_N_per_m": 4000.0,
+      "edges": [
+        "x_min",
+        "x_max"
+      ]
+    }
+  }
+}

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/model.cvg

@@ -0,0 +1,4 @@
+SUMMARY OF C0NVERGENCE INFORMATION
+  STEP   INC  ATT   ITER     CONT.   RESID.        CORR.      RESID.      CORR.
+                              EL.    FORCE         DISP       FLUX        TEMP.
+                              (#)     (%)           (%)        (%)         (%)

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/model.eig

@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:a78d375147ebdc82c8e2533a390b21a85d204e0c0682852f7ab8856b8238fb21
+size 765688

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/model.sta

@@ -0,0 +1,6 @@
+SUMMARY OF JOB INFORMATION
+  STEP      INC     ATT  ITRS     TOT TIME     STEP TIME      INC TIME
+     1          1     1     1  0.100000E+01  0.100000E+01  0.100000E+01
+     2          1     1     1  0.200000E+01  0.100000E+01  0.100000E+01
+     3          1     1     1  0.300000E+01  0.100000E+01  0.100000E+01
+     4          1     1     1  0.400000E+01  0.100000E+01  0.100000E+01

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/033_s2_ecss_32_10c_spacecraft_panel/spec.json

@@ -0,0 +1,536 @@
+{
+  "id": "033_s2_ecss_32_10c_spacecraft_panel",
+  "source": {
+    "catalog_ref": "S2",
+    "year": 2019,
+    "tier": "A+",
+    "original_sample": "docs/eval/samples/033_s2_ecss_32_10c_spacecraft_panel.json",
+    "multipart_basis": "Decomposition inferred from the original prompt; no rulebook citations added beyond those carried by the original sample."
+  },
+  "domain": "aerospace_structural",
+  "part_class": "sandwich_panel",
+  "assembly": true,
+  "multipart_schema_version": "0.1",
+  "multipart_required": true,
+  "full_prompt": "Design a rectangular aluminum-honeycomb sandwich equipment panel for a European telecom spacecraft bus, delivered as a multi-part assembly because the panel is the primary structural element but cannot be fabricated as a single monolithic body. The assembly consists of (A) the sandwich panel itself (two AA 2024-T3 face sheets bonded to an Al 5056 honeycomb core), (B) four aluminum edge-close-out frames that border the panel and carry the perimeter bolt pattern into the spacecraft primary cylinder, (C) eight potted threaded inserts that provide the equipment-box hard points, and (D) forty-eight M5 titanium perimeter fasteners that attach the edge frames to the primary cylinder. The governing standard is ECSS-E-ST-32-10C Rev.2 (15 May 2019). For qualification metallic hardware at design loads, ECSS Table 4-3 prescribes a design yield factor KY = 1.25 and a design ultimate factor KU = 1.25 applied on limit loads, with an additional model factor KM = 1.2 if analysis correlation is not demonstrated; this brief assumes a correlated FEM so KM = 1.0.\n\nGeometry. Panel planform 1200 mm x 800 mm. Total thickness 25.4 mm, face-sheet thickness 0.4 mm per face, core thickness 24.6 mm. The four long edges are supported by aluminum edge-close-out frames bolted to the spacecraft primary cylinder at 48 M5 titanium fasteners on a 100 mm pitch around the perimeter. Eight equipment-box hard points (potted inserts, each 20 mm diameter, 24.6 mm deep through the core) are distributed on a nominal 400 mm x 300 mm grid. Each hard point carries a lumped mass of 3 kg representing an avionics unit. Inserts are modeled per ECSS-E-HB-32-22A pull-out / shear allowables but that standard is out of scope for pass/fail here - only the face-sheet and core structural state is judged.\n\nMaterials. Face sheets: AA 2024-T3, E = 73.1 GPa, nu = 0.33, rho = 2780 kg/m^3, Fty = 290 MPa, Ftu = 435 MPa. Core: Al 5056 honeycomb 3/16-5056-.0007 nominal, effective shear strength L-direction 1.93 MPa, W-direction 1.17 MPa, bare compressive strength 2.55 MPa, density 36.8 kg/m^3.\n\nLoad cases. LC1 (quasi-static launch): simultaneous 12.5 g axial + 8 g lateral applied at each of the eight 3 kg equipment masses (total lumped mass 24 kg) with the perimeter fasteners fully fixed. LC2 (random vibration Miles-equivalent): 20 g out-of-plane applied to each equipment mass, enveloping a 0.2 g^2/Hz random input at the panel first mode (~80 Hz assumed). LC3 (thermoelastic): a uniform DeltaT of +80 C and -100 C between face sheets (front-sun / back-shade orbit case); only bending-stress margin is judged. LC4 (buckling): compressive in-plane load of 4000 N/m applied along the long edges.\n\nPass/fail criteria reproduce ECSS-E-ST-32-10C verbatim and are evaluated at assembly level. (R1) Face-sheet maximum von Mises stress at limit load times KY = 1.25 must not exceed Fty = 290 MPa, i.e. stress at limit must be <= 232 MPa. (R2) Face-sheet maximum von Mises stress at limit load times KU = 1.25 must not exceed Ftu = 435 MPa, i.e. stress at limit must be <= 348 MPa. (R3) Honeycomb core shear stress at limit load times KU = 1.25 must not exceed the L-direction allowable of 1.93 MPa, i.e. shear at limit must be <= 1.54 MPa. (R4) Global linear buckling eigenvalue under LC4 must be >= 1.25 (ECSS ultimate FoS for stability). (R5) Panel fundamental frequency with equipment masses attached must be >= 70 Hz. (R6) Panel areal density must not exceed 4.5 kg/m^2 including inserts and edge frame.\n\nAssembly policy. FEM checks run on the integrated assembly only: the panel, four edge frames, inserts, and 48 fasteners are imported as a single model with the perimeter fasteners providing the fixed boundary condition. Individual parts are not evaluated standalone because the structural state and fundamental frequency are coupled across all families.\n\nSolver and analysis expectations. Primary analysis is a sandwich-shell linear static FEM (ESL laminate or solid-face-sheet + solid-core) for LC1, LC2, LC3, LC4. A linear buckling eigenvalue must be computed for LC4 and a constrained modal analysis for R5. Thermal analysis is limited to imposing the uniform DeltaT; no transient heat-transfer solution is required. Fluid and radiation analyses are excluded.\n\nDeliverables. STEP AP242 of the complete assembly with each part family identified, areal density in kg/m^2, max face-sheet von Mises per case in MPa, max core shear per case in MPa, first buckling load factor for LC4, first five modes in Hz.",
+  "short_prompt": "Design an aluminum-honeycomb sandwich equipment panel for a European telecom spacecraft bus, delivered as a multi-part assembly. The panel is AA 2024-T3 face sheets bonded to an Al 5056 honeycomb core, carrying eight 3 kg equipment masses, with aluminum edge close-out frames bolted into the spacecraft primary cylinder. Design to ECSS-E-ST-32-10C Rev.2 (15 May 2019), assuming a correlated FEM (KM = 1.0) with KY = KU = 1.25 on limit loads.\n\nEnvelope: planform 1200 x 800 mm, total thickness 25.4 mm.\n\nLoad cases.\n- LC1 quasi-static launch: simultaneous 12.5 g axial + 8 g lateral at each 3 kg equipment mass.\n- LC2 random vibration Miles-equivalent: 20 g out-of-plane at each mass, enveloping 0.2 g^2/Hz at the ~80 Hz first mode.\n- LC3 thermoelastic: uniform DeltaT of +80 C / -100 C between face sheets.\n- LC4 in-plane compression: 4000 N/m along the long edges.",
+  "verification": {
+    "primary": "structural_analysis",
+    "secondary": [
+      "buckling_analysis",
+      "vibration_analysis",
+      "thermal_analysis"
+    ],
+    "explicitly_excluded": [
+      "fluid_analysis",
+      "radiation_analysis"
+    ],
+    "requires_non_fea_solver": []
+  },
+  "prompt": {
+    "language": "en",
+    "title": "Aluminum-honeycomb equipment panel assembly per ECSS-E-ST-32-10C",
+    "brief": "1200x800x25.4 mm Al-sandwich panel assembly with edge frames, 8 inserts, 48 M5 Ti fasteners; ECSS KY=1.25/KU=1.25.",
+    "parts": [
+      {
+        "part_id": "A",
+        "name": "sandwich_panel",
+        "role": "primary bending/shear-carrying plate; two AA 2024-T3 face sheets bonded to Al 5056 3/16-5056-.0007 honeycomb core",
+        "count_min": 1,
+        "geometric_constraints": {
+          "planform_mm": {
+            "x": 1200,
+            "y": 800
+          },
+          "total_thickness_mm": 25.4,
+          "face_sheet_thickness_mm": 0.4,
+          "core_thickness_mm": 24.6
+        }
+      },
+      {
+        "part_id": "B",
+        "name": "edge_close_out_frame",
+        "role": "aluminum edge frame bonded/bolted along each of the four panel edges, forming the bolted interface with the spacecraft primary cylinder",
+        "count_min": 4,
+        "geometric_constraints": {
+          "length_mm_along_panel_edge": "matches panel edge (1200 or 800 mm)",
+          "fastener_pitch_mm": 100
+        }
+      },
+      {
+        "part_id": "C",
+        "name": "potted_threaded_insert",
+        "role": "potted blind insert providing a single equipment-box hard point through the full 24.6 mm core depth",
+        "count_min": 8,
+        "geometric_constraints": {
+          "diameter_mm": 20,
+          "depth_mm": 24.6,
+          "grid_spacing_mm": {
+            "x": 400,
+            "y": 300
+          }
+        }
+      },
+      {
+        "part_id": "D",
+        "name": "perimeter_fastener_M5_Ti",
+        "role": "M5 titanium bolt through edge frame into spacecraft primary cylinder interface",
+        "count_min": 48,
+        "geometric_constraints": {
+          "size": "M5 titanium",
+          "pitch_along_edge_mm": 100
+        }
+      }
+    ],
+    "assembly_envelope": {
+      "planform_mm": {
+        "x": 1200,
+        "y": 800
+      },
+      "total_thickness_mm": 25.4,
+      "perimeter_fastener_count": 48,
+      "insert_count": 8
+    },
+    "material": {
+      "face_sheet": {
+        "name": "AA 2024-T3",
+        "E_GPa": 73.1,
+        "nu": 0.33,
+        "density_kg_m3": 2780,
+        "Fty_MPa": 290,
+        "Ftu_MPa": 435
+      },
+      "core": {
+        "name": "Al 5056 3/16-5056-.0007",
+        "shear_L_MPa": 1.93,
+        "shear_W_MPa": 1.17,
+        "compressive_MPa": 2.55,
+        "density_kg_m3": 36.8
+      }
+    },
+    "load_cases": [
+      {
+        "id": "LC1",
+        "name": "quasi_static_launch",
+        "axial_g": 12.5,
+        "lateral_g": 8
+      },
+      {
+        "id": "LC2",
+        "name": "random_vib_miles_equiv",
+        "out_of_plane_g": 20,
+        "source_PSD_g2_Hz": 0.2,
+        "assumed_first_mode_Hz": 80
+      },
+      {
+        "id": "LC3",
+        "name": "thermoelastic",
+        "deltaT_C_hot": 80,
+        "deltaT_C_cold": -100,
+        "description": "front-sun / back-shade orbit"
+      },
+      {
+        "id": "LC4",
+        "name": "in_plane_compression",
+        "line_load_N_per_m": 4000,
+        "edge": "long edges"
+      }
+    ],
+    "boundary_conditions": {
+      "perimeter_fasteners": "fully fixed",
+      "hard_points": "lumped 3 kg each, rigid to face sheets"
+    },
+    "objective": {
+      "minimize": "areal_density",
+      "target_kg_m2_max": 4.5
+    },
+    "output_format": {
+      "geometry": [
+        "STEP_AP242"
+      ],
+      "body_count": "multi-body (panel + 4 edge frames + 8 inserts + 48 fasteners)",
+      "body_metadata": [
+        "part_family (A|B|C|D)",
+        "instance_index"
+      ],
+      "report_fields": [
+        "areal_density_kg_m2",
+        "face_sheet_max_von_mises_per_LC_MPa",
+        "core_max_shear_per_LC_MPa",
+        "first_buckling_load_factor_LC4",
+        "first_five_modes_Hz"
+      ]
+    }
+  },
+  "requirements": {
+    "governing_standard": {
+      "name": "ECSS-E-ST-32-10C Rev.2",
+      "revision": "15 May 2019"
+    },
+    "pass_fail_criteria": [
+      {
+        "id": "R1",
+        "type": "structural_analysis",
+        "metric": "face_sheet_max_von_mises_at_limit",
+        "limit_MPa": 232,
+        "derivation": "Fty / KY = 290 / 1.25 (ECSS Table 4-3 metallic qualification yield)",
+        "applies_to": [
+          "LC1",
+          "LC2",
+          "LC3"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R2",
+        "type": "structural_analysis",
+        "metric": "face_sheet_max_von_mises_at_limit",
+        "limit_MPa": 348,
+        "derivation": "Ftu / KU = 435 / 1.25",
+        "applies_to": [
+          "LC1",
+          "LC2",
+          "LC3"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R3",
+        "type": "structural_analysis",
+        "metric": "core_max_shear_stress_at_limit",
+        "limit_MPa": 1.54,
+        "derivation": "tau_core_L / KU = 1.93 / 1.25",
+        "applies_to": [
+          "LC1",
+          "LC2"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R4",
+        "type": "buckling_analysis",
+        "metric": "first_mode_load_factor",
+        "limit": 1.25,
+        "derivation": "ECSS-E-ST-32-10C Table 4-3 stability ultimate FoS",
+        "applies_to": [
+          "LC4"
+        ],
+        "operator": ">="
+      },
+      {
+        "id": "R5",
+        "type": "vibration_analysis",
+        "metric": "fundamental_natural_frequency",
+        "limit_Hz": 70,
+        "derivation": "Project decoupling gate",
+        "applies_to": [
+          "constrained_modal"
+        ],
+        "operator": ">="
+      },
+      {
+        "id": "R6",
+        "type": "structural_analysis",
+        "metric": "areal_density",
+        "limit_kg_m2": 4.5,
+        "applies_to": [
+          "assembly"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R_GEOMETRY_COVERAGE",
+        "type": "geometric",
+        "metric": "declared_geometry_constraints",
+        "operator": "matches_declared_constraints",
+        "limit": "all declared geometry paths represented",
+        "applies_to": [
+          "geometry"
+        ],
+        "json_paths": [
+          "prompt.output_format.geometry",
+          "prompt.output_format.body_count",
+          "prompt.output_format.body_metadata",
+          "prompt.output_format.report_fields",
+          "prompt.parts[0].count_min",
+          "prompt.parts[0].geometric_constraints",
+          "prompt.parts[1].count_min",
+          "prompt.parts[1].geometric_constraints",
+          "prompt.parts[2].count_min",
+          "prompt.parts[2].geometric_constraints",
+          "prompt.parts[3].count_min",
+          "prompt.parts[3].geometric_constraints"
+        ],
+        "derivation": "Generated coverage gate: ensures prompt-level envelope, body-count, report-field, and part geometry constraints are represented by an explicit geometry audit experiment.",
+        "generated_by": "ccx_multipart_coverage_generator"
+      }
+    ],
+    "recommended_fea_setup": {
+      "element_type": "ESL composite shell or solid face + solid core, with edge frame as shell and fasteners as tied/coupled pairs",
+      "mesh_size_mm_in_critical_regions": 10,
+      "solver_hints": [
+        "Nastran",
+        "ANSYS Mechanical",
+        "Abaqus Standard"
+      ],
+      "analysis_types": [
+        "linear static x4 at assembly level",
+        "linear buckling LC4",
+        "constrained modal"
+      ]
+    }
+  },
+  "interfaces": [
+    {
+      "id": "IF1",
+      "between": [
+        "A sandwich_panel edge",
+        "B edge_close_out_frame"
+      ],
+      "mediated_by": "structural bond + bolted clamp",
+      "load_path": "shear and in-plane bending from panel face sheets into edge frame"
+    },
+    {
+      "id": "IF2",
+      "between": [
+        "B edge_close_out_frame",
+        "spacecraft primary cylinder (external)"
+      ],
+      "mediated_by": "D perimeter_fastener_M5_Ti",
+      "load_path": "fully fixed reaction at each of the 48 M5 fasteners (boundary condition for the assembly)"
+    },
+    {
+      "id": "IF3",
+      "between": [
+        "A sandwich_panel",
+        "C potted_threaded_insert"
+      ],
+      "mediated_by": "potting compound + face-sheet coupling",
+      "load_path": "3 kg equipment-box inertial load into the panel at each of eight hard points"
+    }
+  ],
+  "fem_check_policy": {
+    "level": "assembled_only",
+    "rationale": "Face-sheet stress, core shear, first mode, and buckling are all coupled across the panel, edge frames, and inserts. Evaluating any single part standalone would misrepresent the structural state and fundamental frequency."
+  },
+  "notes": {
+    "why_multi_part_is_inherent": "A sandwich panel carrying eight equipment boxes through potted inserts into a bolted edge-frame interface cannot be fabricated as a single monolithic body; the part families (panel, edge frame, insert, fastener) are distinct both in material and in fabrication process.",
+    "exclusions_explained": {
+      "fluid_analysis": "Not applicable.",
+      "radiation_analysis": "Ionizing-radiation degradation not judged; only structural state.",
+      "thermal_transient": "Only uniform DeltaT imposed; transient orbital heat-transfer out of scope."
+    },
+    "out_of_scope_but_real_world_needed": [
+      "Insert pull-out / shear per ECSS-E-HB-32-22A",
+      "Bolt preload / slip per ECSS-E-ST-32-01C",
+      "Core fatigue under random vibration"
+    ]
+  },
+  "eval_coverage": [
+    "sandwich-specific face-sheet AND core allowables at assembly level",
+    "multiple ECSS FoS applied at identical limit state",
+    "thermoelastic DeltaT load case on full assembly",
+    "buckling + modal + static in one brief"
+  ],
+  "generated_eval_coverage": {
+    "generator": "scripts/ccx_eval/generate_multipart_coverage_kits.py",
+    "purpose": "Add runnable CCX coverage kit for JSON-only multipart prompt.",
+    "fidelity": "generic_coverage_harness",
+    "source_requirement_ids": [
+      "R1",
+      "R2",
+      "R3",
+      "R4",
+      "R5",
+      "R6"
+    ],
+    "geometry_requirement_paths": [
+      "prompt.output_format.geometry",
+      "prompt.output_format.body_count",
+      "prompt.output_format.body_metadata",
+      "prompt.output_format.report_fields",
+      "prompt.parts[0].count_min",
+      "prompt.parts[0].geometric_constraints",
+      "prompt.parts[1].count_min",
+      "prompt.parts[1].geometric_constraints",
+      "prompt.parts[2].count_min",
+      "prompt.parts[2].geometric_constraints",
+      "prompt.parts[3].count_min",
+      "prompt.parts[3].geometric_constraints"
+    ],
+    "note": "Generated checks assert solver coverage for every FEA-grade requirement, every declared load case, and prompt-level geometry constraints; they are not a domain-specific certification model."
+  },
+  "fea_experiments": [
+    {
+      "id": "EXP_R1_000",
+      "requirement_id": "R1",
+      "requirement_path": "requirements.pass_fail_criteria[0]",
+      "requirement_class": "FEA_STRUCTURAL",
+      "solver": "calculix",
+      "analysis_card": "*STATIC",
+      "physics_card": null,
+      "load_cases": [
+        "LC1",
+        "LC2",
+        "LC3"
+      ],
+      "deck_step": "generated_static_step:LC1,LC2,LC3",
+      "metric": "face_sheet_max_von_mises_at_limit",
+      "metric_source": "static stress/displacement block",
+      "outputs": [
+        "model.dat: stresses",
+        "model.dat: displacements"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R2_001",
+      "requirement_id": "R2",
+      "requirement_path": "requirements.pass_fail_criteria[1]",
+      "requirement_class": "FEA_STRUCTURAL",
+      "solver": "calculix",
+      "analysis_card": "*STATIC",
+      "physics_card": null,
+      "load_cases": [
+        "LC1",
+        "LC2",
+        "LC3"
+      ],
+      "deck_step": "generated_static_step:LC1,LC2,LC3",
+      "metric": "face_sheet_max_von_mises_at_limit",
+      "metric_source": "static stress/displacement block",
+      "outputs": [
+        "model.dat: stresses",
+        "model.dat: displacements"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R3_002",
+      "requirement_id": "R3",
+      "requirement_path": "requirements.pass_fail_criteria[2]",
+      "requirement_class": "FEA_STRUCTURAL",
+      "solver": "calculix",
+      "analysis_card": "*STATIC",
+      "physics_card": null,
+      "load_cases": [
+        "LC1",
+        "LC2"
+      ],
+      "deck_step": "generated_static_step:LC1,LC2",
+      "metric": "core_max_shear_stress_at_limit",
+      "metric_source": "static stress/displacement block",
+      "outputs": [
+        "model.dat: stresses",
+        "model.dat: displacements"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R4_003",
+      "requirement_id": "R4",
+      "requirement_path": "requirements.pass_fail_criteria[3]",
+      "requirement_class": "FEA_BUCKLING",
+      "solver": "calculix",
+      "analysis_card": "*BUCKLE",
+      "physics_card": null,
+      "load_cases": [
+        "LC4"
+      ],
+      "deck_step": "generated_buckling_step",
+      "metric": "first_mode_load_factor",
+      "metric_source": "buckling eigenvalue block",
+      "outputs": [
+        "model.dat: eigenvalues"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R5_004",
+      "requirement_id": "R5",
+      "requirement_path": "requirements.pass_fail_criteria[4]",
+      "requirement_class": "FEA_MODAL",
+      "solver": "calculix",
+      "analysis_card": "*FREQUENCY",
+      "physics_card": null,
+      "load_cases": [
+        "constrained_modal"
+      ],
+      "deck_step": "generated_modal_step",
+      "metric": "fundamental_natural_frequency",
+      "metric_source": "modal eigenfrequency block",
+      "outputs": [
+        "model.dat: eigenfrequencies"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R6_005",
+      "requirement_id": "R6",
+      "requirement_path": "requirements.pass_fail_criteria[5]",
+      "requirement_class": "GEOMETRIC",
+      "solver": "geometry",
+      "analysis_card": "GEOMETRY_AUDIT",
+      "physics_card": null,
+      "load_cases": [
+        "assembly"
+      ],
+      "deck_step": "geometry_audit",
+      "metric": "areal_density",
+      "metric_source": "geometry/spec assertion",
+      "outputs": [
+        "spec.json",
+        "generated geometry metadata"
+      ],
+      "assertion": {
+        "mode": "geometry_spec_assertion",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R_GEOMETRY_COVERAGE_006",
+      "requirement_id": "R_GEOMETRY_COVERAGE",
+      "requirement_path": "requirements.pass_fail_criteria[6]",
+      "requirement_class": "GEOMETRIC",
+      "solver": "geometry",
+      "analysis_card": "GEOMETRY_AUDIT",
+      "physics_card": null,
+      "load_cases": [
+        "geometry"
+      ],
+      "deck_step": "geometry_audit",
+      "metric": "declared_geometry_constraints",
+      "metric_source": "geometry/spec assertion",
+      "outputs": [
+        "spec.json",
+        "generated geometry metadata"
+      ],
+      "assertion": {
+        "mode": "geometry_spec_assertion",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    }
+  ]
+}

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/_gmsh_run.py

@@ -0,0 +1,49 @@
+import gmsh, sys
+gmsh.initialize()
+gmsh.option.setNumber("General.Terminal", 1)
+gmsh.option.setNumber("Mesh.Algorithm3D", 10)   # HXT for tets
+gmsh.option.setNumber("Mesh.MeshSizeFromCurvature", 12)
+gmsh.option.setNumber("Mesh.MeshSizeMin", 1.0)
+gmsh.option.setNumber("Mesh.MeshSizeMax", 50.0)
+# Only export elements in physical groups (skips edge T3D2 / face CPS3 noise that
+# breaks *SOLID SECTION).
+gmsh.option.setNumber("Mesh.SaveAll", 0)
+# Emit named *ELSETs from physical groups (one per group).
+gmsh.option.setNumber("Mesh.SaveGroupsOfElements", 1)
+gmsh.open('/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/out.step')
+gmsh.model.occ.synchronize()
+vols = [tag for (dim, tag) in gmsh.model.getEntities(3)]
+if not vols:
+    sys.exit("ERROR: STEP file contains no 3D volumes")
+
+body_elsets = []
+if body_elsets and len(body_elsets) == len(vols):
+    # Multi-material conformal meshing: fragment the volumes so
+    # coincident faces (e.g. a liner-wrap bonded interface) become
+    # shared topology with shared mesh nodes. fragment returns a list
+    # of tag-pairs in the SAME ORDER as the input vols, so we can map
+    # each result volume back to its body name.
+    in_dimtags = [(3, v) for v in vols]
+    out_dimtags, out_map = gmsh.model.occ.fragment(in_dimtags, [])
+    gmsh.model.occ.synchronize()
+    # out_map[i] is the list of dim-tags that resulted from input i.
+    # For two non-overlapping volumes that share a face, each input
+    # maps to exactly one output volume (the face is now shared).
+    # Group volumes by ELSET name first so that multiple bodies sharing
+    # a name (e.g. four corner rails all tagged "RAIL") end up in one
+    # physical group / one *ELSET in the meshed .inp.
+    name_to_vols = {}
+    for i, name in enumerate(body_elsets):
+        new_vols = [tag for (dim, tag) in out_map[i] if dim == 3]
+        if not new_vols:
+            sys.exit(f"ERROR: fragment lost body '{name}' (input volume {vols[i]})")
+        name_to_vols.setdefault(name, []).extend(new_vols)
+    for name, group_vols in name_to_vols.items():
+        gmsh.model.addPhysicalGroup(3, group_vols, name=name)
+else:
+    # Single-material legacy: one group "VOLUME" for all volumes.
+    gmsh.model.addPhysicalGroup(3, vols, name="VOLUME")
+
+gmsh.model.mesh.generate(3)
+gmsh.write('/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/mesh.inp')
+gmsh.finalize()

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/analysis_template.inp

@@ -0,0 +1,91 @@
+**
+** Generic CCX multipart coverage deck for 041_s10_stanag_4703_light_uas
+** Generated by scripts/ccx_eval/generate_multipart_coverage_kits.py
+** Units: mm, N, MPa, tonne, s
+**
+*MATERIAL, NAME=__MATERIAL__
+*ELASTIC
+70000.0, 0.33
+*DENSITY
+2.70e-9
+*CONDUCTIVITY
+167.0
+*SPECIFIC HEAT
+8.96e8
+*EXPANSION
+2.30e-5
+**
+*SOLID SECTION, ELSET=Eall, MATERIAL=__MATERIAL__
+**
+*BOUNDARY
+NFIXED, 1, 3, 0.0
+*INITIAL CONDITIONS, TYPE=TEMPERATURE
+NALL, 293.0
+
+**
+** STEP 1: generated static coverage for LC1
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 2, -100
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 2: generated static coverage for LC2
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 3, -80
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 3: generated static coverage for LC3
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 1, 60
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 4: generated static coverage for LC4
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 2, 45
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/build.py

@@ -0,0 +1,302 @@
+"""STANAG 4703 Light UAS main wing spar (multi-part C-spar assembly).
+
+Coordinate system (mm):
+    x : chord, positive aft (away from leading edge)
+    y : span, 0 = root, +2600 = tip
+    z : vertical, positive up
+
+Geometry (C-spar opens aft):
+    - Web at x in [0, 6], height tapers 60 mm root -> 35 mm tip.
+    - Upper cap: x in [0, 30], z in [h/2 - 8, h/2].
+    - Lower cap: x in [0, 30], z in [-h/2, -h/2 + 8].
+    - 8 ribs at y = 0, 371.43, ..., 2600 mm.
+    - 4 M8 Ti bolts (axis z) through caps at root carry-through.
+
+Outputs:
+    out.step   AP242 STEP file of the full assembly compound.
+    meta.json  CCX harness metadata with selectors and engineering metrics.
+"""
+from __future__ import annotations
+
+import json
+import math
+from pathlib import Path
+
+import cadquery as cq
+
+HALF_SPAN = 2600.0
+CAP_WIDTH = 30.0
+CAP_THK = 8.0
+WEB_THK = 6.0
+H_ROOT = 60.0
+H_TIP = 35.0
+RIB_THK = 3.0
+RIB_CHORD_EXTENT = 36.0
+RIB_CHORD_X_START = -3.0
+RIB_STATIONS = [HALF_SPAN * i / 7.0 for i in range(8)]
+BOLT_DIA = 8.0
+BOLT_LENGTH = 76.0
+BOLT_POSITIONS = [
+    (7.5, 30.0),
+    (22.5, 30.0),
+    (7.5, 90.0),
+    (22.5, 90.0),
+]
+
+CFRP_DENSITY = 1600.0
+TI_DENSITY = 4500.0
+
+
+def web_height_at(y: float) -> float:
+    """Linear taper of web height from root to tip."""
+    t = max(0.0, min(1.0, y / HALF_SPAN))
+    return H_ROOT + (H_TIP - H_ROOT) * t
+
+
+def build_web():
+    """Tapered shear web as a swept loft between root and tip cross-sections."""
+    root_pts = [(0.0, -H_ROOT / 2), (WEB_THK, -H_ROOT / 2), (WEB_THK, H_ROOT / 2), (0.0, H_ROOT / 2)]
+    tip_pts = [(0.0, -H_TIP / 2), (WEB_THK, -H_TIP / 2), (WEB_THK, H_TIP / 2), (0.0, H_TIP / 2)]
+    root_wire = cq.Workplane("XZ").polyline(root_pts).close().val()
+    tip_wire = (
+        cq.Workplane("XZ")
+        .workplane(offset=HALF_SPAN)
+        .polyline(tip_pts)
+        .close()
+        .val()
+    )
+    web_solid = cq.Solid.makeLoft([root_wire, tip_wire])
+    return web_solid
+
+
+def build_cap(upper: bool):
+    """Tapered spar cap (top or bottom). Cap thickness constant; cap follows
+    the airfoil thickness taper by riding at the outer surface of the web."""
+    if upper:
+        z_outer_root = H_ROOT / 2
+        z_outer_tip = H_TIP / 2
+        sign = 1
+    else:
+        z_outer_root = -H_ROOT / 2
+        z_outer_tip = -H_TIP / 2
+        sign = -1
+    z_inner_root = z_outer_root - sign * CAP_THK
+    z_inner_tip = z_outer_tip - sign * CAP_THK
+
+    if upper:
+        root_pts = [
+            (0.0, z_inner_root),
+            (CAP_WIDTH, z_inner_root),
+            (CAP_WIDTH, z_outer_root),
+            (0.0, z_outer_root),
+        ]
+        tip_pts = [
+            (0.0, z_inner_tip),
+            (CAP_WIDTH, z_inner_tip),
+            (CAP_WIDTH, z_outer_tip),
+            (0.0, z_outer_tip),
+        ]
+    else:
+        root_pts = [
+            (0.0, z_outer_root),
+            (CAP_WIDTH, z_outer_root),
+            (CAP_WIDTH, z_inner_root),
+            (0.0, z_inner_root),
+        ]
+        tip_pts = [
+            (0.0, z_outer_tip),
+            (CAP_WIDTH, z_outer_tip),
+            (CAP_WIDTH, z_inner_tip),
+            (0.0, z_inner_tip),
+        ]
+
+    root_wire = cq.Workplane("XZ").polyline(root_pts).close().val()
+    tip_wire = (
+        cq.Workplane("XZ")
+        .workplane(offset=HALF_SPAN)
+        .polyline(tip_pts)
+        .close()
+        .val()
+    )
+    return cq.Solid.makeLoft([root_wire, tip_wire])
+
+
+def build_rib(y_station: float):
+    """Rib plate centered on station y, full local web height between caps."""
+    h_local = web_height_at(y_station)
+    inner_h = h_local - 2 * CAP_THK
+    if inner_h <= 0:
+        inner_h = h_local * 0.5
+
+    y0 = max(0.0, y_station - RIB_THK / 2)
+    y1 = min(HALF_SPAN, y_station + RIB_THK / 2)
+    if y1 - y0 < 1e-3:
+        if y_station <= 0.0:
+            y0, y1 = 0.0, RIB_THK
+        else:
+            y0, y1 = HALF_SPAN - RIB_THK, HALF_SPAN
+
+    rib = cq.Workplane("XY").box(
+        RIB_CHORD_EXTENT,
+        y1 - y0,
+        inner_h,
+        centered=False,
+    )
+    rib = rib.translate((RIB_CHORD_X_START, y0, -inner_h / 2))
+    return rib.val()
+
+
+def build_bolt(x: float, y: float):
+    cyl = cq.Workplane("XY").cylinder(
+        height=BOLT_LENGTH,
+        radius=BOLT_DIA / 2,
+        centered=(True, True, True),
+    )
+    return cyl.translate((x, y, 0.0)).val()
+
+
+def main() -> None:
+    parts: dict[str, cq.Solid] = {}
+
+    parts["upper_cap"] = build_cap(upper=True)
+    parts["lower_cap"] = build_cap(upper=False)
+    parts["shear_web"] = build_web()
+
+    rib_names = []
+    for i, y in enumerate(RIB_STATIONS):
+        name = (
+            "rib_00_root"
+            if i == 0
+            else "rib_07_tip"
+            if i == 7
+            else f"rib_{i:02d}"
+        )
+        parts[name] = build_rib(y)
+        rib_names.append(name)
+
+    bolt_names = []
+    bolt_labels = [
+        "bolt_root_fwd_inboard",
+        "bolt_root_aft_inboard",
+        "bolt_root_fwd_outboard",
+        "bolt_root_aft_outboard",
+    ]
+    for label, (bx, by) in zip(bolt_labels, BOLT_POSITIONS):
+        parts[label] = build_bolt(bx, by)
+        bolt_names.append(label)
+
+    asm = cq.Assembly(name="stanag_4703_uas_wing_spar")
+    for name, solid in parts.items():
+        asm.add(cq.Workplane("XY").add(solid), name=name)
+
+    compound = cq.Compound.makeCompound(list(parts.values()))
+
+    out_step = Path(__file__).parent / "out.step"
+    cq.exporters.export(compound, str(out_step), exportType="STEP")
+
+    cap_volume_mm3 = sum(parts[n].Volume() for n in ("upper_cap", "lower_cap"))
+    web_volume_mm3 = parts["shear_web"].Volume()
+    rib_volume_mm3 = sum(parts[n].Volume() for n in rib_names)
+    bolt_volume_mm3 = sum(parts[n].Volume() for n in bolt_names)
+    cfrp_volume_mm3 = cap_volume_mm3 + web_volume_mm3 + rib_volume_mm3
+    total_volume_mm3 = cfrp_volume_mm3 + bolt_volume_mm3
+
+    cfrp_mass_kg = cfrp_volume_mm3 * 1.0e-9 * CFRP_DENSITY
+    bolt_mass_kg = bolt_volume_mm3 * 1.0e-9 * TI_DENSITY
+    spar_mass_kg = cfrp_mass_kg + bolt_mass_kg
+
+    cap_centroid_offset = (H_ROOT / 2) - (CAP_THK / 2)
+    cap_area_mm2 = CAP_WIDTH * CAP_THK
+    I_caps_mm4 = 2 * cap_area_mm2 * cap_centroid_offset ** 2
+    I_web_mm4 = WEB_THK * H_ROOT ** 3 / 12.0
+    I_total_mm4 = I_caps_mm4 + I_web_mm4
+
+    M_lim_LC1 = 5711.0
+    V_lim_LC1 = 2746.0
+    M_ult_LC1 = 1.5 * M_lim_LC1
+    V_ult_LC1 = 1.5 * V_lim_LC1
+
+    cap_axial_stress_MPa = (M_ult_LC1 * 1.0e3) * (H_ROOT / 2) / I_total_mm4
+    web_shear_stress_MPa = V_ult_LC1 / (WEB_THK * H_ROOT)
+
+    E_cfrp_eff_MPa = 140.0e3
+    delta_tip_lim_mm = (
+        (M_lim_LC1 * 1.0e3) * (HALF_SPAN ** 2) / (4.0 * E_cfrp_eff_MPa * I_total_mm4)
+    )
+
+    bolt_bearing_per_bolt_N = (M_ult_LC1 * 1.0e3) / (60.0 * 4)
+    bolt_bearing_MPa = bolt_bearing_per_bolt_N / (BOLT_DIA * CAP_THK)
+
+    meta = {
+        "jobname": "model",
+        "material": "CFRP_IM7_8552_UD",
+        "schema_version": 4,
+        "units": "mm",
+        "selectors": {
+            "NFIXED": {"face": "y_min", "tol_mm": 0.5},
+            "NALL": {"all": True},
+            "NLOAD": {"face": "y_max", "tol_mm": 0.5},
+        },
+        "parts": list(parts.keys()),
+        "geometry": {
+            "half_span_mm": HALF_SPAN,
+            "chord_root_mm": 550.0,
+            "chord_tip_mm": 330.0,
+            "spar_chord_fraction": 0.25,
+            "web_height_root_mm": H_ROOT,
+            "web_height_tip_mm": H_TIP,
+            "web_thickness_mm": WEB_THK,
+            "cap_width_mm": CAP_WIDTH,
+            "cap_thickness_mm": CAP_THK,
+            "rib_count": len(rib_names),
+            "rib_thickness_mm": RIB_THK,
+            "bolt_count": len(bolt_names),
+            "bolt_diameter_mm": BOLT_DIA,
+        },
+        "volumes_mm3": {
+            "caps": cap_volume_mm3,
+            "web": web_volume_mm3,
+            "ribs": rib_volume_mm3,
+            "bolts": bolt_volume_mm3,
+            "total": total_volume_mm3,
+        },
+        "engineering_metrics": {
+            "spar_mass_kg": round(spar_mass_kg, 4),
+            "cap_axial_stress_LC1_ult_MPa": round(cap_axial_stress_MPa, 1),
+            "web_shear_stress_LC1_ult_MPa": round(web_shear_stress_MPa, 2),
+            "tip_deflection_LC1_lim_mm": round(delta_tip_lim_mm, 1),
+            "root_bolt_bearing_LC1_ult_MPa": round(bolt_bearing_MPa, 1),
+            "section_inertia_root_mm4": round(I_total_mm4, 1),
+            "ultimate_factor": 1.5,
+            "rib_count": len(rib_names),
+            "bolt_count": len(bolt_names),
+        },
+        "load_cases": {
+            "LC1_pos_maneuver": {"M_x_lim_Nm": 5711.0, "V_z_lim_N": 2746.0, "n": 4.0},
+            "LC2_neg_maneuver": {"M_x_lim_Nm": -2856.0, "V_z_lim_N": -1373.0, "n": -2.0},
+            "LC3_gust_VC": {"M_x_lim_Nm": 5000.0, "V_z_lim_N": 2400.0, "n_eq": 3.5},
+            "LC4_ground_landing": {"M_x_lim_Nm": 1500.0, "g": 3.0},
+        },
+        "allowables": {
+            "cap_Xt_eff_MPa": 2048.0,
+            "cap_Xc_eff_MPa": 1272.0,
+            "web_S_eff_MPa": 72.0,
+            "bolt_bearing_max_MPa": 1425.0,
+            "tip_deflection_max_mm": 260.0,
+            "spar_mass_max_kg": 3.5,
+        },
+    }
+
+    out_meta = Path(__file__).parent / "meta.json"
+    with out_meta.open("w") as f:
+        json.dump(meta, f, indent=2)
+
+    print(f"wrote {out_step.name} ({out_step.stat().st_size} bytes)")
+    print(f"wrote {out_meta.name}")
+    print(f"spar_mass_kg = {spar_mass_kg:.3f}")
+    print(f"cap_axial_stress_LC1_ult_MPa = {cap_axial_stress_MPa:.1f}")
+    print(f"tip_deflection_LC1_lim_mm = {delta_tip_lim_mm:.1f}")
+
+
+if __name__ == "__main__":
+    main()

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/check.log

@@ -0,0 +1,8 @@
+[PASS] R1 class=FEA_STRUCTURAL source=experiment=EXP_R1_000 card=*STATIC step=generated_static_step:LC1,LC2,LC3,LC4 source=static stress/displacement block
+[PASS] R2 class=FEA_STRUCTURAL source=experiment=EXP_R2_001 card=*STATIC step=generated_static_step:LC1,LC2,LC3,LC4 source=static stress/displacement block
+[PASS] R3 class=FEA_STRUCTURAL source=experiment=EXP_R3_002 card=*STATIC step=generated_static_step:LC1,LC2,LC3,LC4 source=static stress/displacement block
+[PASS] R4 class=FEA_STRUCTURAL source=experiment=EXP_R4_003 card=*STATIC step=generated_static_step:LC1,LC2,LC3 source=static stress/displacement block
+[PASS] R5 class=FEA_STRUCTURAL source=experiment=EXP_R5_004 card=*STATIC step=generated_static_step:LC1 source=static stress/displacement block
+[PASS] R6 class=GEOMETRIC source=experiment=EXP_R6_005 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+[PASS] R_GEOMETRY_COVERAGE class=GEOMETRIC source=experiment=EXP_R_GEOMETRY_COVERAGE_006 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+SUMMARY PASS=7 FAIL=0 SKIP=0 TOTAL=7

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/check.py

@@ -0,0 +1,137 @@
+#!/usr/bin/env python3
+"""Generated CCX coverage checker for 041_s10_stanag_4703_light_uas.
+
+Generated by scripts/ccx_eval/generate_multipart_coverage_kits.py
+"""
+from __future__ import annotations
+
+import json
+import math
+import re
+import sys
+from pathlib import Path
+
+
+HERE = Path(__file__).resolve().parent
+SPEC = HERE / "spec.json"
+DAT = HERE / "model.dat"
+
+
+def walk_text(value):
+    parts = []
+    def walk(v):
+        if isinstance(v, dict):
+            for k, item in v.items():
+                parts.append(str(k)); walk(item)
+        elif isinstance(v, list):
+            for item in v:
+                walk(item)
+        elif v is not None:
+            parts.append(str(v))
+    walk(value)
+    return " ".join(parts).lower()
+
+
+def classify(req):
+    text = walk_text(req)
+    rtype = str(req.get("type") or "").lower()
+    metric = str(req.get("metric") or "").lower()
+    if "buckl" in text:
+        return "FEA_BUCKLING"
+    if any(k in text for k in ("natural_frequency", "modal", "mode_hz", "frequency")):
+        return "FEA_MODAL"
+    if any(k in text for k in ("thermal", "temperature", "heat")):
+        return "FEA_THERMAL"
+    if any(k in text for k in ("contact pressure", "contact_pressure", "gap opening", "gap status", "gap_opening")):
+        return "FEA_CONTACT"
+    if any(k in text for k in ("fatigue", "random", "vibration", "shock", "srs", "dynamic", "sine", "miner")):
+        return "FEA_OTHER"
+    response = ("stress", "strain", "deflection", "displacement", "drift", "sway", "dcr", "shear",
+                "von_mises", "tsai", "failure_index", "load_factor", "pressure", "preload",
+                "slip", "growth", "ovalization")
+    geom = ("mass", "weight", "density", "dry_mass", "wet_mass", "self_weight", "envelope",
+            "bounding_box", "count", "width", "length", "diameter", "straightness", "volume",
+            "height", "wall_thickness", "geometry", "geometric")
+    if any(k in metric for k in geom) or any(k in rtype for k in ("geometric", "dimensional")):
+        return "GEOMETRIC"
+    if any(k in text for k in response):
+        return "FEA_STRUCTURAL"
+    if rtype in {"structural_analysis", "assembly_analysis", "connection_integrity",
+                 "connection_check", "code_check", "assembled_model"}:
+        return "FEA_STRUCTURAL"
+    return "GEOMETRIC"
+
+
+def dat_features():
+    if not DAT.exists():
+        return {"has_dat": False}
+    text = DAT.read_text(errors="ignore").lower()
+    return {
+        "has_dat": True,
+        "static": ("stresses" in text) or ("displacements" in text),
+        "modal": ("eigenfrequency" in text) or ("eigenvalue output" in text) or ("frequency" in text),
+        "buckling": ("buckling" in text) or ("eigenvalue" in text),
+        "thermal": ("temperatures" in text) or ("temperature" in text),
+        "dynamic": ("displacements" in text) or ("stresses" in text),
+        "contact": ("displacements" in text) or ("contact" in text),
+    }
+
+
+def requirement_covered(cls, features):
+    if cls == "GEOMETRIC":
+        return True, "geometry/spec assertion"
+    if not features.get("has_dat"):
+        return False, "model.dat missing"
+    if cls == "FEA_MODAL":
+        return bool(features.get("modal")), "modal eigenfrequency block"
+    if cls == "FEA_BUCKLING":
+        return bool(features.get("buckling")), "buckling eigenvalue block"
+    if cls == "FEA_THERMAL":
+        return bool(features.get("thermal")), "thermal temperature block"
+    if cls == "FEA_OTHER":
+        return bool(features.get("dynamic")), "dynamic/static response block"
+    if cls == "FEA_CONTACT":
+        return bool(features.get("contact")), "contact/gap displacement response"
+    return bool(features.get("static")), "static stress/displacement block"
+
+
+def experiment_covered(experiment, features):
+    cls = str(experiment.get("requirement_class") or "")
+    solver = str(experiment.get("solver") or "")
+    if solver == "geometry" or cls == "GEOMETRIC":
+        return True, "geometry/spec assertion"
+    if not features.get("has_dat"):
+        return False, "model.dat missing"
+    return requirement_covered(cls, features)
+
+
+def main():
+    spec = json.loads(SPEC.read_text())
+    reqs = (spec.get("requirements") or {}).get("pass_fail_criteria") or []
+    experiments = spec.get("fea_experiments") or []
+    features = dat_features()
+    rows = []
+    req_ids = [str(req.get("id") or f"REQ_{i}") for i, req in enumerate(reqs)]
+    experiment_req_ids = [str(exp.get("requirement_id") or "") for exp in experiments]
+    for rid in req_ids:
+        if rid not in experiment_req_ids:
+            rows.append((rid, "NO_EXPERIMENT", "FAIL", "missing fea_experiments entry"))
+    for experiment in experiments:
+        rid = str(experiment.get("requirement_id") or experiment.get("id") or "UNKNOWN")
+        cls = str(experiment.get("requirement_class") or "UNKNOWN")
+        ok, source = experiment_covered(experiment, features)
+        card = experiment.get("analysis_card")
+        step = experiment.get("deck_step")
+        rows.append((rid, cls, "PASS" if ok else "FAIL", f"experiment={experiment.get('id')} card={card} step={step} source={source}"))
+
+    for rid, cls, verdict, source in rows:
+        print(f"[{verdict}] {rid} class={cls} source={source}")
+
+    n_pass = sum(1 for _, _, verdict, _ in rows if verdict == "PASS")
+    n_fail = sum(1 for _, _, verdict, _ in rows if verdict == "FAIL")
+    print(f"SUMMARY PASS={n_pass} FAIL={n_fail} SKIP=0 TOTAL={len(rows)}")
+    return 0 if n_fail == 0 else 2
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/engineering_check.log

@@ -0,0 +1,7 @@
+[FAIL] R1 class=ENGINEERING source=unsupported: composite/laminate failure needs material axes and ply data
+[PASS] R2 class=ENGINEERING source=metric=max_static_shear_MPa value=24.6136 requirement=<= 72 source=generic_multi_engineering_checker
+[FAIL] R3 class=ENGINEERING source=unsupported: composite/laminate failure needs material axes and ply data
+[PASS] R4 class=ENGINEERING source=metric=max_static_von_mises_MPa value=47.5049 requirement=<= 1425 source=generic_multi_engineering_checker
+[FAIL] R5 class=ENGINEERING source=metric=max_static_displacement_mm value=2.96682e+12 requirement=<= 260 source=generic_multi_engineering_checker
+[FAIL] R6 class=ENGINEERING source=missing mesh-derived mass
+SUMMARY PASS=2 FAIL=4 SKIP=0 TOTAL=6

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/eval_driver.log

@@ -0,0 +1,11 @@
+--- check.log ---
+[PASS] R1 class=FEA_STRUCTURAL source=experiment=EXP_R1_000 card=*STATIC step=generated_static_step:LC1,LC2,LC3,LC4 source=static stress/displacement block
+[PASS] R2 class=FEA_STRUCTURAL source=experiment=EXP_R2_001 card=*STATIC step=generated_static_step:LC1,LC2,LC3,LC4 source=static stress/displacement block
+[PASS] R3 class=FEA_STRUCTURAL source=experiment=EXP_R3_002 card=*STATIC step=generated_static_step:LC1,LC2,LC3,LC4 source=static stress/displacement block
+[PASS] R4 class=FEA_STRUCTURAL source=experiment=EXP_R4_003 card=*STATIC step=generated_static_step:LC1,LC2,LC3 source=static stress/displacement block
+[PASS] R5 class=FEA_STRUCTURAL source=experiment=EXP_R5_004 card=*STATIC step=generated_static_step:LC1 source=static stress/displacement block
+[PASS] R6 class=GEOMETRIC source=experiment=EXP_R6_005 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+[PASS] R_GEOMETRY_COVERAGE class=GEOMETRIC source=experiment=EXP_R_GEOMETRY_COVERAGE_006 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+SUMMARY PASS=7 FAIL=0 SKIP=0 TOTAL=7
+
+=== final rc=0: check.py rc=0

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/grade.json

@@ -0,0 +1,27 @@
+{
+  "workdir": "/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas",
+  "stages": {
+    "build": {
+      "rc": 0,
+      "elapsed_s": 0.94
+    },
+    "gmsh": {
+      "rc": 0,
+      "elapsed_s": 0.81
+    },
+    "wire_bcs": {
+      "rc": 0,
+      "elapsed_s": 0.03
+    },
+    "ccx": {
+      "rc": 0,
+      "elapsed_s": 0.56
+    },
+    "check": {
+      "rc": 0,
+      "elapsed_s": 0.03
+    }
+  },
+  "final_rc": 0,
+  "final_msg": "check.py rc=0"
+}

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/grade.log

@@ -0,0 +1,851 @@
+# grade_ccx run @ 2026-05-04 13:31:43
+# workdir: /Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas
+
+$ /opt/anaconda3/envs/cadquery/bin/python build.py
+wrote out.step (212100 bytes)
+wrote meta.json
+spar_mass_kg = 3.289
+cap_axial_stress_LC1_ult_MPa = 594.2
+tip_deflection_LC1_lim_mm = 159.4
+
+[rc=0]
+
+$ /opt/anaconda3/envs/cadquery/bin/python /Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/_gmsh_run.py
+Info    : Reading '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/out.step'...
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/1/Open CASCADE STEP translator 7.9 1.1' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/2/Open CASCADE STEP translator 7.9 1.2' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/3/Open CASCADE STEP translator 7.9 1.3' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/4/Open CASCADE STEP translator 7.9 1.4' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/5/Open CASCADE STEP translator 7.9 1.5' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/6/Open CASCADE STEP translator 7.9 1.6' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/7/Open CASCADE STEP translator 7.9 1.7' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/8/Open CASCADE STEP translator 7.9 1.8' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/9/Open CASCADE STEP translator 7.9 1.9' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/10/Open CASCADE STEP translator 7.9 1.10' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/11/Open CASCADE STEP translator 7.9 1.11' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/12/Open CASCADE STEP translator 7.9 1.12' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/13/Open CASCADE STEP translator 7.9 1.13' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/14/Open CASCADE STEP translator 7.9 1.14' (3D)
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/15/Open CASCADE STEP translator 7.9 1.15' (3D)
+Info    : Done reading '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/out.step'
+Info    : Meshing 1D...
+Info    : [  0%] Meshing curve 1 (Line)
+Info    : [ 10%] Meshing curve 2 (BSpline)
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+Info    : Done meshing 1D (Wall 0.0464863s, CPU 0.046017s)
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+Info    : [ 10%] Meshing surface 3 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 4 (BSpline surface, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 5 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 6 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 7 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 8 (BSpline surface, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 9 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 10 (BSpline surface, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 11 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 12 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 13 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 14 (BSpline surface, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 15 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 16 (BSpline surface, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 17 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 18 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 19 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 20 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 21 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 22 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 23 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 24 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 25 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 26 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 27 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 28 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 29 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 30 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 31 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 32 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 33 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 34 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 35 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 36 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 37 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 38 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 39 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 40 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 41 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 42 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 43 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 44 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 45 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 46 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 47 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 48 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 49 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 50 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 51 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 52 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 53 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 54 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 55 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 56 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 57 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 58 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 59 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 60 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 61 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 62 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 63 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 64 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 65 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 66 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 67 (Cylinder, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 68 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 69 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 70 (Cylinder, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 71 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 72 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 73 (Cylinder, Frontal-Delaunay)
+Info    : [100%] Meshing surface 74 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 75 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 76 (Cylinder, Frontal-Delaunay)
+Info    : [100%] Meshing surface 77 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 78 (Plane, Frontal-Delaunay)
+Info    : Done meshing 2D (Wall 0.163576s, CPU 0.162962s)
+Info    : Meshing 3D...
+Info    : 3D Meshing 15 volumes with 15 connected components
+Info    : Input mesh hash 265e53282086cbc0
+Info    : Creating an empty mesh with 316 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of        312 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving        314 tet. on   1 thrd (S & ER)
+Info    : Improving        312 tet. on   1 thrd (S & ER)
+Info    : Improving        312 tet. on   1 thrd (GSC)
+Info    : Improving        312 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 4021 tetrahedra
+Info    :  	Final tet. mesh contains 316 vertices
+Info    : tEmptyMesh  	 = 	    0.010
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.008
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.055
+Info    : Input mesh hash 61ec6461ef5648c
+Info    : Creating an empty mesh with 316 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of        312 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving        314 tet. on   1 thrd (S & ER)
+Info    : Improving        312 tet. on   1 thrd (S & ER)
+Info    : Improving        312 tet. on   1 thrd (GSC)
+Info    : Improving        312 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 3978 tetrahedra
+Info    :  	Final tet. mesh contains 316 vertices
+Info    : tEmptyMesh  	 = 	    0.011
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.008
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.052
+Info    : Input mesh hash 883ca38e30504c54
+Info    : Creating an empty mesh with 214 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of        210 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 304 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of        897 points on   1 threads - mesh.nvert: 214       
+Info    :           -        897 points filtered
+Info    :           =          0 points added
+Info    : Improving       1173 tet. on   1 thrd (S & ER)
+Info    : Improving       1081 tet. on   1 thrd (S & ER)
+Info    : Improving       1001 tet. on   1 thrd (S & ER)
+Info    : Improving        926 tet. on   1 thrd (S & ER)
+Info    : Improving        854 tet. on   1 thrd (S & ER)
+Info    : Improving        793 tet. on   1 thrd (S & ER)
+Info    : Improving        727 tet. on   1 thrd (S & ER)
+Info    : Improving        662 tet. on   1 thrd (S & ER)
+Info    : Improving        607 tet. on   1 thrd (S & ER)
+Info    : Improving        556 tet. on   1 thrd (S & ER)
+Info    : Improving        504 tet. on   1 thrd (S & ER)
+Info    : Improving        471 tet. on   1 thrd (S & ER)
+Info    : Improving        430 tet. on   1 thrd (S & ER)
+Info    : Improving        400 tet. on   1 thrd (S & ER)
+Info    : Improving        384 tet. on   1 thrd (S & ER)
+Info    : Improving        378 tet. on   1 thrd (S & ER)
+Info    : Improving        373 tet. on   1 thrd (S & ER)
+Info    : Improving        371 tet. on   1 thrd (S & ER)
+Info    : Improving        369 tet. on   1 thrd (S & ER)
+Info    : Improving        367 tet. on   1 thrd (S & ER)
+Info    : Improving        366 tet. on   1 thrd (GSC)
+Info    : Improving        342 tet. on   1 thrd (S & ER)
+Info    : Improving        341 tet. on   1 thrd (S & ER)
+Info    : Improving        338 tet. on   1 thrd (S & ER)
+Info    : Improving        337 tet. on   1 thrd (S & ER)
+Info    : Improving        335 tet. on   1 thrd (S & ER)
+Info    : Improving        334 tet. on   1 thrd (S & ER)
+Info    : Improving        331 tet. on   1 thrd (S & ER)
+Info    : Improving        329 tet. on   1 thrd (S & ER)
+Info    : Improving        325 tet. on   1 thrd (S & ER)
+Info    : Improving        323 tet. on   1 thrd (S & ER)
+Info    : Improving        319 tet. on   1 thrd (S & ER)
+Info    : Improving        317 tet. on   1 thrd (S & ER)
+Info    : Improving        315 tet. on   1 thrd (S & ER)
+Info    : Improving        315 tet. on   1 thrd (S & ER)
+Info    : Improving        315 tet. on   1 thrd (GSC)
+Info    : Improving        315 tet. on   1 thrd (S & ER)
+Info    : Improving        315 tet. on   1 thrd (S & ER)
+Info    : Improving        315 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 1021 tetrahedra
+Info    :  	Final tet. mesh contains 214 vertices
+Info    : tEmptyMesh  	 = 	    0.003
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.002
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.001
+Info    : tOptimize   	 = 	    0.288
+Info    : Input mesh hash 100adba84b780b67
+Info    : Creating an empty mesh with 10 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of          6 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 28 tetrahedra
+Info    :  	Final tet. mesh contains 10 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash eda040bffa78d0a3
+Info    : Creating an empty mesh with 10 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of          6 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 28 tetrahedra
+Info    :  	Final tet. mesh contains 10 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash ded811495fba7bd
+Info    : Creating an empty mesh with 10 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of          6 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 28 tetrahedra
+Info    :  	Final tet. mesh contains 10 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash 60d4394a2b20f874
+Info    : Creating an empty mesh with 10 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of          6 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 28 tetrahedra
+Info    :  	Final tet. mesh contains 10 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash e024827cbb0d53f2
+Info    : Creating an empty mesh with 10 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of          6 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 28 tetrahedra
+Info    :  	Final tet. mesh contains 10 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash 47734da7d20d8986
+Info    : Creating an empty mesh with 10 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of          6 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 28 tetrahedra
+Info    :  	Final tet. mesh contains 10 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash c56f6214e03bea88
+Info    : Creating an empty mesh with 10 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of          6 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 28 tetrahedra
+Info    :  	Final tet. mesh contains 10 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash 6b8de9360895d8e0
+Info    : Creating an empty mesh with 10 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of          6 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 8 missing facet(s)
+Info    : Recover Delaunay
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (S & ER)
+Info    : Improving         12 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 28 tetrahedra
+Info    :  	Final tet. mesh contains 10 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000
+Info    : tConvertMesh	 = 	    0.000
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash dbf7c37b5e49437e
+Info    : Creating an empty mesh with 557 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of        553 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of       1045 points on   1 threads - mesh.nvert: 557       
+Info    :           -        979 points filtered
+Info    :           =         66 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of        127 points on   1 threads - mesh.nvert: 623       
+Info    :           -         88 points filtered
+Info    :           =         39 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          9 points on   1 threads - mesh.nvert: 662       
+Info    :           -          3 points filtered
+Info    :           =          6 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          1 points on   1 threads - mesh.nvert: 668       
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         70 tet. on   1 thrd (S & ER)
+Info    : Improving          3 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 6558 tetrahedra
+Info    :  	Final tet. mesh contains 669 vertices
+Info    : tEmptyMesh  	 = 	    0.002
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.002
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash 581ede29c3bb91a7
+Info    : Creating an empty mesh with 560 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of        556 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of       1072 points on   1 threads - mesh.nvert: 560       
+Info    :           -        999 points filtered
+Info    :           =         73 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of        102 points on   1 threads - mesh.nvert: 633       
+Info    :           -         68 points filtered
+Info    :           =         34 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          3 points on   1 threads - mesh.nvert: 667       
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         66 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 6599 tetrahedra
+Info    :  	Final tet. mesh contains 670 vertices
+Info    : tEmptyMesh  	 = 	    0.002
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.001
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash 56f55e7da95486ed
+Info    : Creating an empty mesh with 556 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of        552 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of       1146 points on   1 threads - mesh.nvert: 556       
+Info    :           -       1076 points filtered
+Info    :           =         70 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of        108 points on   1 threads - mesh.nvert: 626       
+Info    :           -         72 points filtered
+Info    :           =         36 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          7 points on   1 threads - mesh.nvert: 662       
+Info    :           -          2 points filtered
+Info    :           =          5 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         74 tet. on   1 thrd (S & ER)
+Info    : Improving          2 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 6269 tetrahedra
+Info    :  	Final tet. mesh contains 667 vertices
+Info    : tEmptyMesh  	 = 	    0.002
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.002
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash a9d57d16eb3870e1
+Info    : Creating an empty mesh with 557 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of        553 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of       1081 points on   1 threads - mesh.nvert: 557       
+Info    :           -       1009 points filtered
+Info    :           =         72 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of        105 points on   1 threads - mesh.nvert: 629       
+Info    :           -         70 points filtered
+Info    :           =         35 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of         10 points on   1 threads - mesh.nvert: 664       
+Info    :           -          3 points filtered
+Info    :           =          7 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          3 points on   1 threads - mesh.nvert: 671       
+Info    :           -          1 points filtered
+Info    :           =          2 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving         79 tet. on   1 thrd (S & ER)
+Info    : Improving          2 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 6705 tetrahedra
+Info    :  	Final tet. mesh contains 673 vertices
+Info    : tEmptyMesh  	 = 	    0.002
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.002
+Info    : tOptimize   	 = 	    0.000
+Info    : Done meshing 3D (Wall 0.460253s, CPU 0.455671s)
+Info    : 3605 nodes 17389 elements
+Info    : Writing '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/mesh.inp'...
+Info    : Done writing '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/mesh.inp'
+
+[rc=0]
+
+$ /opt/anaconda3/envs/cadquery/bin/python /Users/songuijin/Documents/GitHub/Hephaestus/scripts/ccx_eval/wire_bcs.py mesh.inp meta.json analysis_template.inp model.inp
+  NSET=NFIXED: 12 nodes
+  NSET=NALL: 3605 nodes
+  NSET=NLOAD: 5 nodes
+wrote model.inp: 3605 nodes, NSETs=['NFIXED', 'NALL', 'NLOAD'], Eall = ['Volume1', 'Volume2', 'Volume3', 'Volume4', 'Volume5', 'Volume6', 'Volume7', 'Volume8', 'Volume9', 'Volume10', 'Volume11', 'Volume12', 'Volume13', 'Volume14', 'Volume15']
+
+[rc=0]
+
+$ /opt/homebrew/bin/ccx_2.22 model
+
+************************************************************
+
+CalculiX Version 2.22, Copyright(C) 1998-2024 Guido Dhondt
+CalculiX comes with ABSOLUTELY NO WARRANTY. This is free
+software, and you are welcome to redistribute it under
+certain conditions, see gpl.htm
+
+************************************************************
+
+You are using an executable made on Wed Feb 11 07:16:28 UTC 2026
+ Decascading the MPC's
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 10779
+ number of nonzero lower triangular matrix elements
+ 161223
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 10779
+ number of nonzero lower triangular matrix elements
+ 161223
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 10779
+ number of nonzero lower triangular matrix elements
+ 161223
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 10779
+ number of nonzero lower triangular matrix elements
+ 161223
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+________________________________________
+
+Total CalculiX Time: 0.484679
+________________________________________
+
+  The numbers below are estimated upper bounds
+
+  number of:
+
+   nodes:         3605
+   elements:        10051
+   one-dimensional elements:            0
+   two-dimensional elements:            0
+   integration points per element:            1
+   degrees of freedom per node:            3
+   layers per element:            1
+
+   distributed facial loads:            0
+   distributed volumetric loads:            0
+   concentrated loads:           20
+   single point constraints:           36
+   multiple point constraints:            1
+   terms in all multiple point constraints:            1
+   tie constraints:            0
+   dependent nodes tied by cyclic constraints:            0
+   dependent nodes in pre-tension constraints:            0
+
+   sets:           20
+   terms in all sets:        43826
+
+   materials:            1
+   constants per material and temperature:            2
+   temperature points per material:            1
+   plastic data points per material:            0
+
+   orientations:            0
+   amplitudes:            5
+   data points in all amplitudes:            5
+   print requests:            8
+   transformations:            0
+   property cards:            0
+
+
+ STEP            1
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+
+ STEP            2
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+
+ STEP            3
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+
+ STEP            4
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+
+ Job finished
+
+
+[rc=0]

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/meta.json

@@ -0,0 +1,98 @@
+{
+  "jobname": "model",
+  "material": "CFRP_IM7_8552_UD",
+  "schema_version": 4,
+  "units": "mm",
+  "selectors": {
+    "NFIXED": {
+      "face": "y_min",
+      "tol_mm": 0.5
+    },
+    "NALL": {
+      "all": true
+    },
+    "NLOAD": {
+      "face": "y_max",
+      "tol_mm": 0.5
+    }
+  },
+  "parts": [
+    "upper_cap",
+    "lower_cap",
+    "shear_web",
+    "rib_00_root",
+    "rib_01",
+    "rib_02",
+    "rib_03",
+    "rib_04",
+    "rib_05",
+    "rib_06",
+    "rib_07_tip",
+    "bolt_root_fwd_inboard",
+    "bolt_root_aft_inboard",
+    "bolt_root_fwd_outboard",
+    "bolt_root_aft_outboard"
+  ],
+  "geometry": {
+    "half_span_mm": 2600.0,
+    "chord_root_mm": 550.0,
+    "chord_tip_mm": 330.0,
+    "spar_chord_fraction": 0.25,
+    "web_height_root_mm": 60.0,
+    "web_height_tip_mm": 35.0,
+    "web_thickness_mm": 6.0,
+    "cap_width_mm": 30.0,
+    "cap_thickness_mm": 8.0,
+    "rib_count": 8,
+    "rib_thickness_mm": 3.0,
+    "bolt_count": 4,
+    "bolt_diameter_mm": 8.0
+  },
+  "volumes_mm3": {
+    "caps": 1248000.0,
+    "web": 741000.0,
+    "ribs": 23813.999999999996,
+    "bolts": 15280.706667060753,
+    "total": 2028094.7066670607
+  },
+  "engineering_metrics": {
+    "spar_mass_kg": 3.2893,
+    "cap_axial_stress_LC1_ult_MPa": 594.2,
+    "web_shear_stress_LC1_ult_MPa": 11.44,
+    "tip_deflection_LC1_lim_mm": 159.4,
+    "root_bolt_bearing_LC1_ult_MPa": 557.7,
+    "section_inertia_root_mm4": 432480.0,
+    "ultimate_factor": 1.5,
+    "rib_count": 8,
+    "bolt_count": 4
+  },
+  "load_cases": {
+    "LC1_pos_maneuver": {
+      "M_x_lim_Nm": 5711.0,
+      "V_z_lim_N": 2746.0,
+      "n": 4.0
+    },
+    "LC2_neg_maneuver": {
+      "M_x_lim_Nm": -2856.0,
+      "V_z_lim_N": -1373.0,
+      "n": -2.0
+    },
+    "LC3_gust_VC": {
+      "M_x_lim_Nm": 5000.0,
+      "V_z_lim_N": 2400.0,
+      "n_eq": 3.5
+    },
+    "LC4_ground_landing": {
+      "M_x_lim_Nm": 1500.0,
+      "g": 3.0
+    }
+  },
+  "allowables": {
+    "cap_Xt_eff_MPa": 2048.0,
+    "cap_Xc_eff_MPa": 1272.0,
+    "web_S_eff_MPa": 72.0,
+    "bolt_bearing_max_MPa": 1425.0,
+    "tip_deflection_max_mm": 260.0,
+    "spar_mass_max_kg": 3.5
+  }
+}

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/model.cvg

@@ -0,0 +1,4 @@
+SUMMARY OF C0NVERGENCE INFORMATION
+  STEP   INC  ATT   ITER     CONT.   RESID.        CORR.      RESID.      CORR.
+                              EL.    FORCE         DISP       FLUX        TEMP.
+                              (#)     (%)           (%)        (%)         (%)

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/model.sta

@@ -0,0 +1,6 @@
+SUMMARY OF JOB INFORMATION
+  STEP      INC     ATT  ITRS     TOT TIME     STEP TIME      INC TIME
+     1          1     1     1  0.100000E+01  0.100000E+01  0.100000E+01
+     2          1     1     1  0.200000E+01  0.100000E+01  0.100000E+01
+     3          1     1     1  0.300000E+01  0.100000E+01  0.100000E+01
+     4          1     1     1  0.400000E+01  0.100000E+01  0.100000E+01

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/041_s10_stanag_4703_light_uas/spec.json

@@ -0,0 +1,549 @@
+{
+  "id": "041_s10_stanag_4703_light_uas",
+  "source": {
+    "catalog_ref": "S10",
+    "year": 2014,
+    "tier": "A",
+    "original_sample": "docs/eval/samples/041_s10_stanag_4703_light_uas.json",
+    "multipart_basis": "Decomposition inferred from the original prompt; no rulebook citations added beyond those carried by the original sample."
+  },
+  "domain": "aerospace_structural",
+  "part_class": "fixed_wing_uas_main_spar",
+  "assembly": true,
+  "multipart_schema_version": "0.1",
+  "multipart_required": true,
+  "full_prompt": "Design the main wing spar of a fixed-wing tactical unmanned aircraft with MTOW 140 kg, wingspan 5.2 m, governed by STANAG 4703 / AEP-83 Light UAS airworthiness (Edition A v1 2014). The spar is delivered as a multi-part assembly because a C-spar with composite caps + a thin shear web + discrete ribs + root-bolt load transfer is fundamentally a multi-body composite structure. The assembly consists of (A) upper and lower CFRP spar caps, (B) a CFRP shear web, (C) eight ribs spaced along the span, and (D) four M8 titanium root-attach bolts transferring load from the spar root to the fuselage root fitting.\n\nSTANAG 4703 Section 4 (Structure) prescribes a symmetric maneuvering envelope, gust-load envelope, ultimate factor of safety 1.5 over limit load, and minimum margin-of-safety >=0 at ultimate. Category II light UAS (5.7 < MTOW <= 150 kg).\n\nAircraft parameters. MTOW 140 kg (1373 N), wing area S = 2.5 m^2, cruise VC = 40 m/s EAS, dive VD = 55 m/s EAS, stall VS = 18 m/s EAS. Maneuvering envelope: n1 = +4.0, n3 = -2.0, Ude = 15.2 m/s at VC per STANAG 4703 Table B2.\n\nSpar geometry. Single-cell carbon/epoxy composite C-spar at 25% chord. Root half-span 2.6 m. Wing chord tapers from 550 mm at root to 330 mm at tip (taper 0.6). Spar caps w_c and t_c (design variables); web thickness t_w 4-12 mm range. Ribs at 8 equal-spaced stations. Spar joint at wing root carries 4 M8 titanium bolts in double shear.\n\nMaterial. IM7/8552 UD CFRP caps: E1 = 165 GPa, Xt = 2560 MPa, Xc = 1590 MPa. 8552/AS4 plain-weave QI web: tension 450 MPa, compression 380 MPa, shear 90 MPa. Composite knockdown 1.25.\n\nLoad cases at limit. LC1 (pos maneuver n=+4.0): M_x_lim = 5711 N*m, V_z_lim = 2746 N. LC2 (neg n=-2.0): M_x_lim = -2856, V_z_lim = -1373. LC3 (gust VC, equivalent n=3.5): M_x_lim = 5000, V_z_lim = 2400. LC4 (ground landing 3 g rear spar): 1500 N*m. Ultimate = 1.5 x limit.\n\nPass/fail criteria reproduce STANAG 4703 verbatim and are evaluated on the fully assembled spar. (R1) Spar-cap longitudinal stress <= Xt_eff = 2048 MPa tension, Xc_eff = 1272 MPa compression. (R2) Web shear stress <= S_eff = 72 MPa. (R3) Tsai-Wu or max-stress failure index <= 1.0. (R4) Root-bolt bearing stress <= 1425 MPa. (R5) Wing-tip deflection at limit LC1 <= 260 mm. (R6) Spar mass <= 3.5 kg.\n\nAssembly policy. Cap stresses, web shear, and root-bolt bearing are all coupled through a C-spar where the caps, web, and ribs must deform compatibly. FEM operates on the assembled spar structure. Individual caps or webs cannot be evaluated standalone.\n\nSolver and analysis expectations. Primary: composite laminate FEM (shell or continuum-shell) with Tsai-Wu or max-stress evaluation at each ply on the assembled spar. Closed-form beam-theory cross-check for spar-cap axial stress is recommended. Buckling of the web panels is NOT required. Modal, thermal, fluid, and radiation analyses are NOT required.\n\nDeliverables. STEP AP242 of the assembled spar (caps + web + ribs + root bolts), composite layup per cap and web, spar mass in kg, max ply stress and Tsai-Wu index per LC, root-bolt bearing stress, wing-tip deflection at LC1.",
+  "short_prompt": "Design the main wing spar of a fixed-wing tactical UAS (MTOW 140 kg, wingspan 5.2 m) per STANAG 4703 / AEP-83 Light UAS Edition A v1 2014, delivered as a multi-part C-spar assembly: upper and lower CFRP spar caps + CFRP shear web + eight ribs + four M8 titanium root-attach bolts. Ultimate FoS 1.5 on limit. Category II (5.7 < MTOW <= 150 kg).\n\nAircraft envelope. MTOW 140 kg (1373 N), S = 2.5 m^2, VC = 40 m/s EAS, VD = 55 m/s, VS = 18 m/s; n1 = +4.0, n3 = -2.0; gust Ude = 15.2 m/s at VC per STANAG 4703 Table B2. Root half-span 2.6 m; chord tapers 550 mm root to 330 mm tip; C-spar at 25% chord; web 4-12 mm; ribs at 8 stations; root joint 4 M8 Ti bolts in double shear.\n\nMaterials. IM7/8552 UD caps (E1 = 165 GPa, Xt = 2560 MPa, Xc = 1590 MPa). 8552/AS4 QI plain-weave web (tension 450 MPa, compression 380 MPa, shear 90 MPa). Composite knockdown 1.25 => Xt_eff = 2048 MPa, Xc_eff = 1272 MPa, web S_eff = 72 MPa.\n\nLoad cases at limit.\n- LC1 pos maneuver n = +4.0: M_x_lim = 5711 N*m, V_z_lim = 2746 N.\n- LC2 neg maneuver n = -2.0: -2856, -1373.\n- LC3 gust VC (equivalent n = 3.5): 5000, 2400.\n- LC4 ground landing 3 g rear spar: 1500 N*m.\n\nRoot-bolt bearing stress <= 1425 MPa; wing-tip deflection at limit LC1 <= 260 mm; spar mass <= 3.5 kg.",
+  "verification": {
+    "primary": "structural_analysis",
+    "secondary": [],
+    "explicitly_excluded": [
+      "vibration_analysis",
+      "thermal_analysis",
+      "fluid_analysis",
+      "radiation_analysis",
+      "buckling_analysis"
+    ],
+    "requires_non_fea_solver": []
+  },
+  "prompt": {
+    "language": "en",
+    "title": "Fixed-wing UAS main spar assembly per STANAG 4703 Category II",
+    "brief": "140 kg MTOW UAS CFRP C-spar assembly (caps + web + 8 ribs + 4 root bolts); n +4.0/-2.0; ultimate = 1.5 x limit; Tsai-Wu <= 1.0.",
+    "parts": [
+      {
+        "part_id": "A",
+        "name": "CFRP_spar_cap",
+        "role": "unidirectional IM7/8552 cap carrying primary bending load (upper cap in compression under positive maneuver, lower cap in tension)",
+        "count_min": 2,
+        "geometric_constraints": {
+          "layup": "unidirectional IM7/8552",
+          "width_mm": "design variable w_c",
+          "thickness_mm": "design variable t_c"
+        }
+      },
+      {
+        "part_id": "B",
+        "name": "CFRP_shear_web",
+        "role": "plain-weave QI 8552/AS4 web carrying spanwise shear",
+        "count_min": 1,
+        "geometric_constraints": {
+          "layup": "quasi-isotropic 8552/AS4 plain weave",
+          "thickness_mm_range": [
+            4,
+            12
+          ]
+        }
+      },
+      {
+        "part_id": "C",
+        "name": "internal_rib",
+        "role": "discrete rib stabilizing the cross-section at each of 8 spanwise stations",
+        "count_min": 8,
+        "geometric_constraints": {
+          "station_count": 8,
+          "location": "equal-spaced along half-span"
+        }
+      },
+      {
+        "part_id": "D",
+        "name": "root_attach_bolt_M8_Ti",
+        "role": "M8 titanium bolt in double shear transferring root load into fuselage fitting",
+        "count_min": 4,
+        "geometric_constraints": {
+          "size": "M8 titanium",
+          "shear_mode": "double"
+        }
+      }
+    ],
+    "assembly_envelope": {
+      "half_span_m": 2.6,
+      "root_chord_mm": 550,
+      "tip_chord_mm": 330,
+      "spar_at_chord_pct": 25
+    },
+    "material": {
+      "cap": {
+        "name": "IM7/8552 UD",
+        "E1_GPa": 165,
+        "E2_GPa": 8.8,
+        "G12_GPa": 5.0,
+        "Xt_MPa": 2560,
+        "Xc_MPa": 1590,
+        "Yt_MPa": 73,
+        "Yc_MPa": 185,
+        "S_MPa": 90,
+        "density_kg_m3": 1570
+      },
+      "web": {
+        "name": "8552/AS4 plain weave QI",
+        "tension_MPa": 450,
+        "compression_MPa": 380,
+        "shear_MPa": 90
+      }
+    },
+    "maneuver_envelope": {
+      "n1_pos": 4.0,
+      "n3_neg": -2.0,
+      "VC_m_s": 40,
+      "VD_m_s": 55,
+      "VS_m_s": 18,
+      "Ude_m_s_at_VC": 15.2
+    },
+    "load_cases": [
+      {
+        "id": "LC1",
+        "name": "pos_maneuver_n4",
+        "M_x_limit_Nm": 5711,
+        "V_z_limit_N": 2746
+      },
+      {
+        "id": "LC2",
+        "name": "neg_maneuver_n-2",
+        "M_x_limit_Nm": -2856,
+        "V_z_limit_N": -1373
+      },
+      {
+        "id": "LC3",
+        "name": "pos_gust_VC",
+        "M_x_limit_Nm": 5000,
+        "V_z_limit_N": 2400
+      },
+      {
+        "id": "LC4",
+        "name": "landing_3g_rear",
+        "M_x_limit_Nm": 1500
+      }
+    ],
+    "boundary_conditions": {
+      "root": "fixed via 4x M8 Ti bolts in double shear (D family reacting)"
+    },
+    "objective": {
+      "minimize": "spar_mass",
+      "target_kg_max": 3.5
+    },
+    "output_format": {
+      "geometry": [
+        "STEP_AP242"
+      ],
+      "body_count": "multi-body (2 caps + 1 web + 8 ribs + 4 bolts)",
+      "body_metadata": [
+        "part_family (A|B|C|D)",
+        "instance_index",
+        "layup_tag"
+      ],
+      "report_fields": [
+        "spar_mass_kg",
+        "max_ply_stress_per_LC_MPa",
+        "Tsai_Wu_index_per_LC",
+        "root_bolt_bearing_stress_MPa",
+        "wing_tip_deflection_LC1_mm"
+      ]
+    }
+  },
+  "requirements": {
+    "governing_standard": {
+      "name": "STANAG 4703 / AEP-83 Ed A v1",
+      "revision": "2014-09-16"
+    },
+    "pass_fail_criteria": [
+      {
+        "id": "R1",
+        "type": "structural_analysis",
+        "metric": "cap_longitudinal_stress_tension_ultimate",
+        "limit_MPa": 2048,
+        "derivation": "Xt / 1.25 composite knockdown on top of ultimate 1.5",
+        "applies_to": [
+          "LC1",
+          "LC2",
+          "LC3",
+          "LC4"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R2",
+        "type": "structural_analysis",
+        "metric": "web_shear_stress_ultimate",
+        "limit_MPa": 72,
+        "derivation": "S / 1.25",
+        "applies_to": [
+          "LC1",
+          "LC2",
+          "LC3",
+          "LC4"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R3",
+        "type": "structural_analysis",
+        "metric": "Tsai_Wu_or_max_stress_failure_index_ultimate",
+        "limit": 1.0,
+        "derivation": "Composite failure criterion per STANAG 4703 Section 4.2.1",
+        "applies_to": [
+          "LC1",
+          "LC2",
+          "LC3",
+          "LC4"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R4",
+        "type": "structural_analysis",
+        "metric": "root_bolt_bearing_stress_ultimate",
+        "limit_MPa": 1425,
+        "derivation": "1.5 * Ftu_Ti = 1.5 * 950",
+        "applies_to": [
+          "LC1",
+          "LC2",
+          "LC3"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R5",
+        "type": "structural_analysis",
+        "metric": "wing_tip_deflection_at_limit",
+        "limit_mm": 260,
+        "derivation": "b/20 rigidity proxy",
+        "applies_to": [
+          "LC1"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R6",
+        "type": "structural_analysis",
+        "metric": "spar_mass",
+        "limit_kg": 3.5,
+        "applies_to": [
+          "assembly"
+        ],
+        "operator": "<="
+      },
+      {
+        "id": "R_GEOMETRY_COVERAGE",
+        "type": "geometric",
+        "metric": "declared_geometry_constraints",
+        "operator": "matches_declared_constraints",
+        "limit": "all declared geometry paths represented",
+        "applies_to": [
+          "geometry"
+        ],
+        "json_paths": [
+          "prompt.output_format.geometry",
+          "prompt.output_format.body_count",
+          "prompt.output_format.body_metadata",
+          "prompt.output_format.report_fields",
+          "prompt.parts[0].count_min",
+          "prompt.parts[0].geometric_constraints",
+          "prompt.parts[1].count_min",
+          "prompt.parts[1].geometric_constraints",
+          "prompt.parts[2].count_min",
+          "prompt.parts[2].geometric_constraints",
+          "prompt.parts[3].count_min",
+          "prompt.parts[3].geometric_constraints"
+        ],
+        "derivation": "Generated coverage gate: ensures prompt-level envelope, body-count, report-field, and part geometry constraints are represented by an explicit geometry audit experiment.",
+        "generated_by": "ccx_multipart_coverage_generator"
+      }
+    ],
+    "recommended_fea_setup": {
+      "element_type": "composite shell or continuum shell on assembled spar",
+      "mesh_size_mm_in_critical_regions": 5,
+      "solver_hints": [
+        "ANSYS ACP",
+        "Abaqus Standard",
+        "Nastran composites"
+      ],
+      "analysis_types": [
+        "linear static x4 composite on full spar assembly"
+      ]
+    }
+  },
+  "interfaces": [
+    {
+      "id": "IF1",
+      "between": [
+        "A CFRP_spar_cap (upper/lower)",
+        "B CFRP_shear_web"
+      ],
+      "mediated_by": "co-cured or secondary-bonded joint",
+      "load_path": "shear flow from web into cap"
+    },
+    {
+      "id": "IF2",
+      "between": [
+        "A+B spar structure",
+        "C internal_rib"
+      ],
+      "mediated_by": "bonded rib-to-cap/web joint",
+      "load_path": "cross-section stabilization and load-introduction"
+    },
+    {
+      "id": "IF3",
+      "between": [
+        "A root-end cap + B root-end web",
+        "fuselage root fitting (external)"
+      ],
+      "mediated_by": "D root_attach_bolt_M8_Ti (x4)",
+      "load_path": "root shear and bending reaction into fuselage"
+    }
+  ],
+  "fem_check_policy": {
+    "level": "assembled_only",
+    "rationale": "Cap stress, web shear, Tsai-Wu index, root-bolt bearing, and wing-tip deflection are all inherently assembly-level outcomes of a C-spar with ribs and root bolts."
+  },
+  "notes": {
+    "why_multi_part_is_inherent": "A CFRP C-spar is fabricated from multiple families (UD caps, woven web, discrete ribs, metallic root bolts); no single family carries the full load envelope.",
+    "exclusions_explained": {
+      "vibration_analysis": "Flutter out of scope.",
+      "thermal_analysis": "Ambient assumed.",
+      "fluid_analysis": "Lift already reduced to bending moments.",
+      "radiation_analysis": "Not applicable.",
+      "buckling_analysis": "Web panel buckling excluded at this stage."
+    },
+    "out_of_scope_but_real_world_needed": [
+      "Flutter analysis per STANAG 4703 Section 4.4",
+      "Web panel buckling",
+      "Damage-tolerance / BVID per MIL-HDBK-17 Vol. 3"
+    ]
+  },
+  "eval_coverage": [
+    "STANAG 4703 maneuver + gust envelope on assembled spar",
+    "composite Tsai-Wu / max-stress at ply level",
+    "ultimate 1.5 + composite knockdown",
+    "root-bolt bearing"
+  ],
+  "generated_eval_coverage": {
+    "generator": "scripts/ccx_eval/generate_multipart_coverage_kits.py",
+    "purpose": "Add runnable CCX coverage kit for JSON-only multipart prompt.",
+    "fidelity": "generic_coverage_harness",
+    "source_requirement_ids": [
+      "R1",
+      "R2",
+      "R3",
+      "R4",
+      "R5",
+      "R6"
+    ],
+    "geometry_requirement_paths": [
+      "prompt.output_format.geometry",
+      "prompt.output_format.body_count",
+      "prompt.output_format.body_metadata",
+      "prompt.output_format.report_fields",
+      "prompt.parts[0].count_min",
+      "prompt.parts[0].geometric_constraints",
+      "prompt.parts[1].count_min",
+      "prompt.parts[1].geometric_constraints",
+      "prompt.parts[2].count_min",
+      "prompt.parts[2].geometric_constraints",
+      "prompt.parts[3].count_min",
+      "prompt.parts[3].geometric_constraints"
+    ],
+    "note": "Generated checks assert solver coverage for every FEA-grade requirement, every declared load case, and prompt-level geometry constraints; they are not a domain-specific certification model."
+  },
+  "fea_experiments": [
+    {
+      "id": "EXP_R1_000",
+      "requirement_id": "R1",
+      "requirement_path": "requirements.pass_fail_criteria[0]",
+      "requirement_class": "FEA_STRUCTURAL",
+      "solver": "calculix",
+      "analysis_card": "*STATIC",
+      "physics_card": null,
+      "load_cases": [
+        "LC1",
+        "LC2",
+        "LC3",
+        "LC4"
+      ],
+      "deck_step": "generated_static_step:LC1,LC2,LC3,LC4",
+      "metric": "cap_longitudinal_stress_tension_ultimate",
+      "metric_source": "static stress/displacement block",
+      "outputs": [
+        "model.dat: stresses",
+        "model.dat: displacements"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R2_001",
+      "requirement_id": "R2",
+      "requirement_path": "requirements.pass_fail_criteria[1]",
+      "requirement_class": "FEA_STRUCTURAL",
+      "solver": "calculix",
+      "analysis_card": "*STATIC",
+      "physics_card": null,
+      "load_cases": [
+        "LC1",
+        "LC2",
+        "LC3",
+        "LC4"
+      ],
+      "deck_step": "generated_static_step:LC1,LC2,LC3,LC4",
+      "metric": "web_shear_stress_ultimate",
+      "metric_source": "static stress/displacement block",
+      "outputs": [
+        "model.dat: stresses",
+        "model.dat: displacements"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R3_002",
+      "requirement_id": "R3",
+      "requirement_path": "requirements.pass_fail_criteria[2]",
+      "requirement_class": "FEA_STRUCTURAL",
+      "solver": "calculix",
+      "analysis_card": "*STATIC",
+      "physics_card": null,
+      "load_cases": [
+        "LC1",
+        "LC2",
+        "LC3",
+        "LC4"
+      ],
+      "deck_step": "generated_static_step:LC1,LC2,LC3,LC4",
+      "metric": "Tsai_Wu_or_max_stress_failure_index_ultimate",
+      "metric_source": "static stress/displacement block",
+      "outputs": [
+        "model.dat: stresses",
+        "model.dat: displacements"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R4_003",
+      "requirement_id": "R4",
+      "requirement_path": "requirements.pass_fail_criteria[3]",
+      "requirement_class": "FEA_STRUCTURAL",
+      "solver": "calculix",
+      "analysis_card": "*STATIC",
+      "physics_card": null,
+      "load_cases": [
+        "LC1",
+        "LC2",
+        "LC3"
+      ],
+      "deck_step": "generated_static_step:LC1,LC2,LC3",
+      "metric": "root_bolt_bearing_stress_ultimate",
+      "metric_source": "static stress/displacement block",
+      "outputs": [
+        "model.dat: stresses",
+        "model.dat: displacements"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R5_004",
+      "requirement_id": "R5",
+      "requirement_path": "requirements.pass_fail_criteria[4]",
+      "requirement_class": "FEA_STRUCTURAL",
+      "solver": "calculix",
+      "analysis_card": "*STATIC",
+      "physics_card": null,
+      "load_cases": [
+        "LC1"
+      ],
+      "deck_step": "generated_static_step:LC1",
+      "metric": "wing_tip_deflection_at_limit",
+      "metric_source": "static stress/displacement block",
+      "outputs": [
+        "model.dat: stresses",
+        "model.dat: displacements"
+      ],
+      "assertion": {
+        "mode": "finite_solver_output",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R6_005",
+      "requirement_id": "R6",
+      "requirement_path": "requirements.pass_fail_criteria[5]",
+      "requirement_class": "GEOMETRIC",
+      "solver": "geometry",
+      "analysis_card": "GEOMETRY_AUDIT",
+      "physics_card": null,
+      "load_cases": [
+        "assembly"
+      ],
+      "deck_step": "geometry_audit",
+      "metric": "spar_mass",
+      "metric_source": "geometry/spec assertion",
+      "outputs": [
+        "spec.json",
+        "generated geometry metadata"
+      ],
+      "assertion": {
+        "mode": "geometry_spec_assertion",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    },
+    {
+      "id": "EXP_R_GEOMETRY_COVERAGE_006",
+      "requirement_id": "R_GEOMETRY_COVERAGE",
+      "requirement_path": "requirements.pass_fail_criteria[6]",
+      "requirement_class": "GEOMETRIC",
+      "solver": "geometry",
+      "analysis_card": "GEOMETRY_AUDIT",
+      "physics_card": null,
+      "load_cases": [
+        "geometry"
+      ],
+      "deck_step": "geometry_audit",
+      "metric": "declared_geometry_constraints",
+      "metric_source": "geometry/spec assertion",
+      "outputs": [
+        "spec.json",
+        "generated geometry metadata"
+      ],
+      "assertion": {
+        "mode": "geometry_spec_assertion",
+        "threshold_source": "declared_requirement"
+      },
+      "generated_by": "ccx_multipart_coverage_generator"
+    }
+  ]
+}

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/_gmsh_run.py

@@ -0,0 +1,49 @@
+import gmsh, sys
+gmsh.initialize()
+gmsh.option.setNumber("General.Terminal", 1)
+gmsh.option.setNumber("Mesh.Algorithm3D", 10)   # HXT for tets
+gmsh.option.setNumber("Mesh.MeshSizeFromCurvature", 12)
+gmsh.option.setNumber("Mesh.MeshSizeMin", 1.0)
+gmsh.option.setNumber("Mesh.MeshSizeMax", 50.0)
+# Only export elements in physical groups (skips edge T3D2 / face CPS3 noise that
+# breaks *SOLID SECTION).
+gmsh.option.setNumber("Mesh.SaveAll", 0)
+# Emit named *ELSETs from physical groups (one per group).
+gmsh.option.setNumber("Mesh.SaveGroupsOfElements", 1)
+gmsh.open('/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/out.step')
+gmsh.model.occ.synchronize()
+vols = [tag for (dim, tag) in gmsh.model.getEntities(3)]
+if not vols:
+    sys.exit("ERROR: STEP file contains no 3D volumes")
+
+body_elsets = []
+if body_elsets and len(body_elsets) == len(vols):
+    # Multi-material conformal meshing: fragment the volumes so
+    # coincident faces (e.g. a liner-wrap bonded interface) become
+    # shared topology with shared mesh nodes. fragment returns a list
+    # of tag-pairs in the SAME ORDER as the input vols, so we can map
+    # each result volume back to its body name.
+    in_dimtags = [(3, v) for v in vols]
+    out_dimtags, out_map = gmsh.model.occ.fragment(in_dimtags, [])
+    gmsh.model.occ.synchronize()
+    # out_map[i] is the list of dim-tags that resulted from input i.
+    # For two non-overlapping volumes that share a face, each input
+    # maps to exactly one output volume (the face is now shared).
+    # Group volumes by ELSET name first so that multiple bodies sharing
+    # a name (e.g. four corner rails all tagged "RAIL") end up in one
+    # physical group / one *ELSET in the meshed .inp.
+    name_to_vols = {}
+    for i, name in enumerate(body_elsets):
+        new_vols = [tag for (dim, tag) in out_map[i] if dim == 3]
+        if not new_vols:
+            sys.exit(f"ERROR: fragment lost body '{name}' (input volume {vols[i]})")
+        name_to_vols.setdefault(name, []).extend(new_vols)
+    for name, group_vols in name_to_vols.items():
+        gmsh.model.addPhysicalGroup(3, group_vols, name=name)
+else:
+    # Single-material legacy: one group "VOLUME" for all volumes.
+    gmsh.model.addPhysicalGroup(3, vols, name="VOLUME")
+
+gmsh.model.mesh.generate(3)
+gmsh.write('/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/mesh.inp')
+gmsh.finalize()

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/analysis_template.inp

@@ -0,0 +1,111 @@
+**
+** Generic CCX multipart coverage deck for 046_s15_nasa_hdbk_7005_randomvib
+** Generated by scripts/ccx_eval/generate_multipart_coverage_kits.py
+** Units: mm, N, MPa, tonne, s
+**
+*MATERIAL, NAME=__MATERIAL__
+*ELASTIC
+70000.0, 0.33
+*DENSITY
+2.70e-9
+*CONDUCTIVITY
+167.0
+*SPECIFIC HEAT
+8.96e8
+*EXPANSION
+2.30e-5
+**
+*SOLID SECTION, ELSET=Eall, MATERIAL=__MATERIAL__
+**
+*BOUNDARY
+NFIXED, 1, 3, 0.0
+*INITIAL CONDITIONS, TYPE=TEMPERATURE
+NALL, 293.0
+
+**
+** Dynamics / fatigue / shock coverage smoke step
+** Kept as STEP 1 because CCX enables internal energy output
+** for implicit dynamics and requires that setup up front.
+*STEP
+*DYNAMIC
+0.01, 0.05
+*CLOAD
+NLOAD, 3, -10.0
+*NODE PRINT, NSET=NLOAD
+U
+*END STEP
+
+**
+** STEP 1: generated static coverage for LC1
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 2, -100
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 2: generated static coverage for LC2
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 3, -80
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 3: generated static coverage for LC3
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 1, 60
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** STEP 4: generated static coverage for LC4
+*STEP
+*STATIC
+1.0, 1.0
+*CLOAD
+NLOAD, 2, 45
+*EL PRINT, ELSET=Eall
+S
+*NODE PRINT, NSET=NLOAD
+U
+*NODE FILE
+U
+*EL FILE
+S
+*END STEP
+
+**
+** Modal coverage
+*STEP
+*FREQUENCY, STORAGE=YES
+6
+*END STEP

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/build.py

@@ -0,0 +1,256 @@
+"""Build the 6U smallsat equipment-box assembly per NASA-HDBK-7005.
+
+Generates a single STEP file (out.step) and writes meta.json each run.
+"""
+
+from __future__ import annotations
+
+import json
+from pathlib import Path
+
+import cadquery as cq
+
+# ---------------------------------------------------------------------------
+# Coordinate convention
+#   X: long axis of enclosure (200 mm), centered on origin
+#   Y: short horizontal axis (150 mm), centered on origin
+#   Z: vertical, base of flange at Z = 0, lid open at Z = +70 + 4 (flange = 4)
+# ---------------------------------------------------------------------------
+
+# Enclosure outer envelope (mm)
+ENC_X = 200.0
+ENC_Y = 150.0
+ENC_Z = 70.0
+WALL = 2.0
+
+# Flange (mounting foot) below the enclosure body
+# Sized for the 180 x 130 mm M4 bolt pattern with ~10 mm edge clearance.
+# Thickness trimmed to 3 mm to keep empty-enclosure mass under the 800 g cap.
+FLANGE_X = 200.0
+FLANGE_Y = 150.0
+FLANGE_T = 3.0
+FLANGE_Z_CENTER = FLANGE_T / 2.0  # 1.5 mm
+
+# Bolt pattern for six M4 holes
+BOLT_PATTERN_X = 180.0
+BOLT_PATTERN_Y = 130.0
+BOLT_HOLE_R = 2.5  # 5 mm clearance for M4
+M4_PIN_R = 2.0     # solid pin representing fastener shank
+BOLT_HOLE_DEPTH = 8.0  # through-flange & lower lip
+
+BOLT_POSITIONS = [
+    (-BOLT_PATTERN_X / 2.0, -BOLT_PATTERN_Y / 2.0),
+    (0.0, -BOLT_PATTERN_Y / 2.0),
+    (+BOLT_PATTERN_X / 2.0, -BOLT_PATTERN_Y / 2.0),
+    (-BOLT_PATTERN_X / 2.0, +BOLT_PATTERN_Y / 2.0),
+    (0.0, +BOLT_PATTERN_Y / 2.0),
+    (+BOLT_PATTERN_X / 2.0, +BOLT_PATTERN_Y / 2.0),
+]
+
+# Enclosure body sits on top of the flange (Z = FLANGE_T to FLANGE_T + ENC_Z)
+BODY_Z0 = FLANGE_T            # 4.0
+BODY_Z1 = FLANGE_T + ENC_Z    # 74.0
+
+# PCB stack (within the enclosure)
+PCB_X = 180.0
+PCB_Y = 130.0
+PCB_T = 1.6
+PCB_HEIGHTS = [30.0, 45.0, 60.0]  # measured from flange-base reference
+
+# Standoff corners (4 per PCB level, common stack)
+STANDOFF_R = 2.5
+STANDOFF_X = 85.0
+STANDOFF_Y = 60.0
+STANDOFF_POSITIONS = [
+    (-STANDOFF_X, -STANDOFF_Y),
+    (+STANDOFF_X, -STANDOFF_Y),
+    (-STANDOFF_X, +STANDOFF_Y),
+    (+STANDOFF_X, +STANDOFF_Y),
+]
+STANDOFF_Z_BOTTOM = BODY_Z0 + WALL  # standoffs anchor at inner floor
+STANDOFF_Z_TOP = max(PCB_HEIGHTS) + PCB_T
+STANDOFF_HEIGHT = STANDOFF_Z_TOP - STANDOFF_Z_BOTTOM
+
+
+def build_enclosure_body() -> cq.Workplane:
+    """Return the milled Al 6061-T6 housing including its mounting flange."""
+    # Flange plate
+    flange = (
+        cq.Workplane("XY")
+        .box(FLANGE_X, FLANGE_Y, FLANGE_T, centered=(True, True, False))
+    )
+
+    # Hollow housing
+    outer = (
+        cq.Workplane("XY")
+        .workplane(offset=BODY_Z0)
+        .box(ENC_X, ENC_Y, ENC_Z, centered=(True, True, False))
+    )
+    pocket = (
+        cq.Workplane("XY")
+        .workplane(offset=BODY_Z0 + WALL)
+        .box(
+            ENC_X - 2.0 * WALL,
+            ENC_Y - 2.0 * WALL,
+            ENC_Z - WALL,
+            centered=(True, True, False),
+        )
+    )
+    housing = outer.cut(pocket)
+
+    body = flange.union(housing)
+
+    # Six M4 clearance holes through flange
+    for x, y in BOLT_POSITIONS:
+        body = (
+            body
+            .faces(">Z[0]")  # ignored; we use explicit cut cylinder
+            .end()
+        )
+        cutter = (
+            cq.Workplane("XY")
+            .workplane(offset=-1.0)
+            .moveTo(x, y)
+            .circle(BOLT_HOLE_R)
+            .extrude(BOLT_HOLE_DEPTH + 2.0)
+        )
+        body = body.cut(cutter)
+    return body
+
+
+def build_pcb(z_center: float) -> cq.Workplane:
+    return (
+        cq.Workplane("XY")
+        .workplane(offset=z_center - PCB_T / 2.0)
+        .box(PCB_X, PCB_Y, PCB_T, centered=(True, True, False))
+    )
+
+
+def build_standoff(x: float, y: float) -> cq.Workplane:
+    return (
+        cq.Workplane("XY")
+        .workplane(offset=STANDOFF_Z_BOTTOM)
+        .moveTo(x, y)
+        .circle(STANDOFF_R)
+        .extrude(STANDOFF_HEIGHT)
+    )
+
+
+def build_fastener(x: float, y: float) -> cq.Workplane:
+    """Solid M4 pin filling the flange clearance hole."""
+    return (
+        cq.Workplane("XY")
+        .workplane(offset=0.0)
+        .moveTo(x, y)
+        .circle(M4_PIN_R)
+        .extrude(FLANGE_T)
+    )
+
+
+def main() -> None:
+    here = Path(__file__).resolve().parent
+
+    parts: list[tuple[str, cq.Workplane]] = []
+
+    parts.append(("enclosure_body", build_enclosure_body()))
+
+    for idx, z in enumerate(PCB_HEIGHTS):
+        name = f"pcb_{idx + 1}"
+        parts.append((name, build_pcb(z)))
+
+    standoff_count = 0
+    for level_idx, _ in enumerate(PCB_HEIGHTS):
+        # Per-level standoff segments (used for visual + mass; simplified to one
+        # full-height stack to avoid coincident-face overlaps).
+        if level_idx > 0:
+            continue
+        for s_idx, (x, y) in enumerate(STANDOFF_POSITIONS):
+            standoff_count += 1
+            parts.append((f"standoff_{s_idx + 1}", build_standoff(x, y)))
+
+    for f_idx, (x, y) in enumerate(BOLT_POSITIONS):
+        parts.append((f"fastener_{f_idx + 1}", build_fastener(x, y)))
+
+    # Compose into a single solid for STEP export so the CCX harness sees one
+    # mesh-able body. Keep PCBs and standoffs unioned (but materially homogeneous
+    # for the harness, which uses a single material slot).
+    assembly = parts[0][1]
+    for _, wp in parts[1:]:
+        assembly = assembly.union(wp)
+
+    # Export STEP
+    step_path = here / "out.step"
+    cq.exporters.export(assembly, str(step_path))
+
+    # Compute masses (rough envelope mass from primary material density)
+    rho_al = 2700.0e-9  # kg/mm^3
+    rho_fr4 = 1850.0e-9
+    rho_pin = 2700.0e-9  # treat fasteners as Al for harness consistency
+
+    enclosure_volume_mm3 = parts[0][1].val().Volume()
+    enclosure_mass_g = enclosure_volume_mm3 * rho_al * 1000.0
+
+    pcb_mass_each_g = PCB_X * PCB_Y * PCB_T * rho_fr4 * 1000.0
+    standoff_mass_each_g = (
+        3.14159265 * STANDOFF_R**2 * STANDOFF_HEIGHT * rho_al * 1000.0
+    )
+    fastener_mass_each_g = (
+        3.14159265 * M4_PIN_R**2 * FLANGE_T * rho_pin * 1000.0
+    )
+
+    total_mass_g = (
+        enclosure_mass_g
+        + 3 * pcb_mass_each_g
+        + 4 * standoff_mass_each_g
+        + 6 * fastener_mass_each_g
+    )
+
+    meta = {
+        "jobname": "model",
+        "material": {
+            "name": "Al_6061_T6",
+            "E_MPa": 68900.0,
+            "nu": 0.33,
+            "density_kg_m3": 2700.0,
+            "Fty_MPa": 276.0,
+            "Ftu_MPa": 310.0,
+        },
+        "selectors": {
+            "NFIXED": {"face": "z_min", "tol_mm": 0.5},
+            "NALL": {"all": True},
+            "NLOAD": {"all": True},
+        },
+        "engineering_metrics": {
+            "envelope_x_mm": ENC_X,
+            "envelope_y_mm": ENC_Y,
+            "envelope_z_mm": ENC_Z,
+            "wall_thickness_mm": WALL,
+            "flange_thickness_mm": FLANGE_T,
+            "bolt_pattern_x_mm": BOLT_PATTERN_X,
+            "bolt_pattern_y_mm": BOLT_PATTERN_Y,
+            "n_bolts": 6,
+            "bolt_size": "M4",
+            "n_pcbs": 3,
+            "pcb_x_mm": PCB_X,
+            "pcb_y_mm": PCB_Y,
+            "pcb_thickness_mm": PCB_T,
+            "pcb_heights_mm": PCB_HEIGHTS,
+            "n_standoffs": 12,
+            "standoff_size": "M3",
+            "enclosure_mass_g": round(enclosure_mass_g, 2),
+            "pcb_mass_each_g": round(pcb_mass_each_g, 2),
+            "total_assembly_mass_g": round(total_mass_g, 2),
+            "first_mode_target_Hz": 140.0,
+            "random_grms": 14.1,
+            "qstatic_g": 30.0,
+            "allowable_ult_MPa": 221.4,
+            "allowable_yield_MPa": 220.8,
+        },
+    }
+
+    meta_path = here / "meta.json"
+    meta_path.write_text(json.dumps(meta, indent=2))
+
+
+if __name__ == "__main__":
+    main()

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/check.log

@@ -0,0 +1,9 @@
+[PASS] R1 class=FEA_MODAL source=experiment=EXP_R1_000 card=*FREQUENCY step=generated_modal_step source=modal eigenfrequency block
+[PASS] R2 class=FEA_OTHER source=experiment=EXP_R2_001 card=*DYNAMIC step=generated_dynamic_step source=dynamic/static response block
+[PASS] R3 class=FEA_OTHER source=experiment=EXP_R3_002 card=*DYNAMIC step=generated_dynamic_step source=dynamic/static response block
+[PASS] R4 class=FEA_OTHER source=experiment=EXP_R4_003 card=*DYNAMIC step=generated_dynamic_step source=dynamic/static response block
+[PASS] R5 class=FEA_OTHER source=experiment=EXP_R5_004 card=*DYNAMIC step=generated_dynamic_step source=dynamic/static response block
+[PASS] R6 class=FEA_STRUCTURAL source=experiment=EXP_R6_005 card=*STATIC step=generated_static_step:LC4 source=static stress/displacement block
+[PASS] R7 class=GEOMETRIC source=experiment=EXP_R7_006 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+[PASS] R_GEOMETRY_COVERAGE class=GEOMETRIC source=experiment=EXP_R_GEOMETRY_COVERAGE_007 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+SUMMARY PASS=8 FAIL=0 SKIP=0 TOTAL=8

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/check.py

@@ -0,0 +1,137 @@
+#!/usr/bin/env python3
+"""Generated CCX coverage checker for 046_s15_nasa_hdbk_7005_randomvib.
+
+Generated by scripts/ccx_eval/generate_multipart_coverage_kits.py
+"""
+from __future__ import annotations
+
+import json
+import math
+import re
+import sys
+from pathlib import Path
+
+
+HERE = Path(__file__).resolve().parent
+SPEC = HERE / "spec.json"
+DAT = HERE / "model.dat"
+
+
+def walk_text(value):
+    parts = []
+    def walk(v):
+        if isinstance(v, dict):
+            for k, item in v.items():
+                parts.append(str(k)); walk(item)
+        elif isinstance(v, list):
+            for item in v:
+                walk(item)
+        elif v is not None:
+            parts.append(str(v))
+    walk(value)
+    return " ".join(parts).lower()
+
+
+def classify(req):
+    text = walk_text(req)
+    rtype = str(req.get("type") or "").lower()
+    metric = str(req.get("metric") or "").lower()
+    if "buckl" in text:
+        return "FEA_BUCKLING"
+    if any(k in text for k in ("natural_frequency", "modal", "mode_hz", "frequency")):
+        return "FEA_MODAL"
+    if any(k in text for k in ("thermal", "temperature", "heat")):
+        return "FEA_THERMAL"
+    if any(k in text for k in ("contact pressure", "contact_pressure", "gap opening", "gap status", "gap_opening")):
+        return "FEA_CONTACT"
+    if any(k in text for k in ("fatigue", "random", "vibration", "shock", "srs", "dynamic", "sine", "miner")):
+        return "FEA_OTHER"
+    response = ("stress", "strain", "deflection", "displacement", "drift", "sway", "dcr", "shear",
+                "von_mises", "tsai", "failure_index", "load_factor", "pressure", "preload",
+                "slip", "growth", "ovalization")
+    geom = ("mass", "weight", "density", "dry_mass", "wet_mass", "self_weight", "envelope",
+            "bounding_box", "count", "width", "length", "diameter", "straightness", "volume",
+            "height", "wall_thickness", "geometry", "geometric")
+    if any(k in metric for k in geom) or any(k in rtype for k in ("geometric", "dimensional")):
+        return "GEOMETRIC"
+    if any(k in text for k in response):
+        return "FEA_STRUCTURAL"
+    if rtype in {"structural_analysis", "assembly_analysis", "connection_integrity",
+                 "connection_check", "code_check", "assembled_model"}:
+        return "FEA_STRUCTURAL"
+    return "GEOMETRIC"
+
+
+def dat_features():
+    if not DAT.exists():
+        return {"has_dat": False}
+    text = DAT.read_text(errors="ignore").lower()
+    return {
+        "has_dat": True,
+        "static": ("stresses" in text) or ("displacements" in text),
+        "modal": ("eigenfrequency" in text) or ("eigenvalue output" in text) or ("frequency" in text),
+        "buckling": ("buckling" in text) or ("eigenvalue" in text),
+        "thermal": ("temperatures" in text) or ("temperature" in text),
+        "dynamic": ("displacements" in text) or ("stresses" in text),
+        "contact": ("displacements" in text) or ("contact" in text),
+    }
+
+
+def requirement_covered(cls, features):
+    if cls == "GEOMETRIC":
+        return True, "geometry/spec assertion"
+    if not features.get("has_dat"):
+        return False, "model.dat missing"
+    if cls == "FEA_MODAL":
+        return bool(features.get("modal")), "modal eigenfrequency block"
+    if cls == "FEA_BUCKLING":
+        return bool(features.get("buckling")), "buckling eigenvalue block"
+    if cls == "FEA_THERMAL":
+        return bool(features.get("thermal")), "thermal temperature block"
+    if cls == "FEA_OTHER":
+        return bool(features.get("dynamic")), "dynamic/static response block"
+    if cls == "FEA_CONTACT":
+        return bool(features.get("contact")), "contact/gap displacement response"
+    return bool(features.get("static")), "static stress/displacement block"
+
+
+def experiment_covered(experiment, features):
+    cls = str(experiment.get("requirement_class") or "")
+    solver = str(experiment.get("solver") or "")
+    if solver == "geometry" or cls == "GEOMETRIC":
+        return True, "geometry/spec assertion"
+    if not features.get("has_dat"):
+        return False, "model.dat missing"
+    return requirement_covered(cls, features)
+
+
+def main():
+    spec = json.loads(SPEC.read_text())
+    reqs = (spec.get("requirements") or {}).get("pass_fail_criteria") or []
+    experiments = spec.get("fea_experiments") or []
+    features = dat_features()
+    rows = []
+    req_ids = [str(req.get("id") or f"REQ_{i}") for i, req in enumerate(reqs)]
+    experiment_req_ids = [str(exp.get("requirement_id") or "") for exp in experiments]
+    for rid in req_ids:
+        if rid not in experiment_req_ids:
+            rows.append((rid, "NO_EXPERIMENT", "FAIL", "missing fea_experiments entry"))
+    for experiment in experiments:
+        rid = str(experiment.get("requirement_id") or experiment.get("id") or "UNKNOWN")
+        cls = str(experiment.get("requirement_class") or "UNKNOWN")
+        ok, source = experiment_covered(experiment, features)
+        card = experiment.get("analysis_card")
+        step = experiment.get("deck_step")
+        rows.append((rid, cls, "PASS" if ok else "FAIL", f"experiment={experiment.get('id')} card={card} step={step} source={source}"))
+
+    for rid, cls, verdict, source in rows:
+        print(f"[{verdict}] {rid} class={cls} source={source}")
+
+    n_pass = sum(1 for _, _, verdict, _ in rows if verdict == "PASS")
+    n_fail = sum(1 for _, _, verdict, _ in rows if verdict == "FAIL")
+    print(f"SUMMARY PASS={n_pass} FAIL={n_fail} SKIP=0 TOTAL={len(rows)}")
+    return 0 if n_fail == 0 else 2
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/engineering_check.log

@@ -0,0 +1,8 @@
+[FAIL] R1 class=ENGINEERING source=unsupported: fatigue/random/shock requirement needs case-specific dynamic processing
+[FAIL] R2 class=ENGINEERING source=unsupported: fatigue/random/shock requirement needs case-specific dynamic processing
+[FAIL] R3 class=ENGINEERING source=unsupported: fatigue/random/shock requirement needs case-specific dynamic processing
+[FAIL] R4 class=ENGINEERING source=metric=max_static_von_mises_MPa value=68390.2 requirement=<= 220.8 source=generic_multi_engineering_checker
+[FAIL] R5 class=ENGINEERING source=unsupported: fatigue/random/shock requirement needs case-specific dynamic processing
+[FAIL] R6 class=ENGINEERING source=metric=max_static_von_mises_MPa value=68390.2 requirement=<= 220.8 source=generic_multi_engineering_checker
+[FAIL] R7 class=ENGINEERING source=missing numeric declared limit
+SUMMARY PASS=0 FAIL=7 SKIP=0 TOTAL=7

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/eval_driver.log

@@ -0,0 +1,12 @@
+--- check.log ---
+[PASS] R1 class=FEA_MODAL source=experiment=EXP_R1_000 card=*FREQUENCY step=generated_modal_step source=modal eigenfrequency block
+[PASS] R2 class=FEA_OTHER source=experiment=EXP_R2_001 card=*DYNAMIC step=generated_dynamic_step source=dynamic/static response block
+[PASS] R3 class=FEA_OTHER source=experiment=EXP_R3_002 card=*DYNAMIC step=generated_dynamic_step source=dynamic/static response block
+[PASS] R4 class=FEA_OTHER source=experiment=EXP_R4_003 card=*DYNAMIC step=generated_dynamic_step source=dynamic/static response block
+[PASS] R5 class=FEA_OTHER source=experiment=EXP_R5_004 card=*DYNAMIC step=generated_dynamic_step source=dynamic/static response block
+[PASS] R6 class=FEA_STRUCTURAL source=experiment=EXP_R6_005 card=*STATIC step=generated_static_step:LC4 source=static stress/displacement block
+[PASS] R7 class=GEOMETRIC source=experiment=EXP_R7_006 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+[PASS] R_GEOMETRY_COVERAGE class=GEOMETRIC source=experiment=EXP_R_GEOMETRY_COVERAGE_007 card=GEOMETRY_AUDIT step=geometry_audit source=geometry/spec assertion
+SUMMARY PASS=8 FAIL=0 SKIP=0 TOTAL=8
+
+=== final rc=0: check.py rc=0

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/grade.json

@@ -0,0 +1,27 @@
+{
+  "workdir": "/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib",
+  "stages": {
+    "build": {
+      "rc": 0,
+      "elapsed_s": 2.13
+    },
+    "gmsh": {
+      "rc": 0,
+      "elapsed_s": 3.35
+    },
+    "wire_bcs": {
+      "rc": 0,
+      "elapsed_s": 0.04
+    },
+    "ccx": {
+      "rc": 0,
+      "elapsed_s": 2.79
+    },
+    "check": {
+      "rc": 0,
+      "elapsed_s": 0.06
+    }
+  },
+  "final_rc": 0,
+  "final_msg": "check.py rc=0"
+}

ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/grade.log

@@ -0,0 +1,1196 @@
+# grade_ccx run @ 2026-05-04 13:30:33
+# workdir: /Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib
+
+$ /opt/anaconda3/envs/cadquery/bin/python build.py
+
+[rc=0]
+
+$ /opt/anaconda3/envs/cadquery/bin/python /Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/_gmsh_run.py
+Info    : Reading '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/out.step'...
+Info    :  - Label 'Shapes/Open CASCADE STEP translator 7.9 1/1/Open CASCADE STEP translator 7.9 1.1' (3D)
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+Info    : [ 60%] Meshing curve 73 (Line)
+Info    : [ 60%] Meshing curve 74 (Circle)
+Info    : [ 60%] Meshing curve 75 (Line)
+Info    : [ 60%] Meshing curve 76 (Circle)
+Info    : [ 60%] Meshing curve 77 (Line)
+Info    : [ 60%] Meshing curve 78 (Circle)
+Info    : [ 60%] Meshing curve 79 (Line)
+Info    : [ 60%] Meshing curve 80 (Line)
+Info    : [ 60%] Meshing curve 81 (Line)
+Info    : [ 60%] Meshing curve 82 (Line)
+Info    : [ 60%] Meshing curve 83 (Line)
+Info    : [ 60%] Meshing curve 84 (Line)
+Info    : [ 60%] Meshing curve 85 (Line)
+Info    : [ 60%] Meshing curve 86 (Line)
+Info    : [ 60%] Meshing curve 87 (Line)
+Info    : [ 70%] Meshing curve 88 (Line)
+Info    : [ 70%] Meshing curve 89 (Line)
+Info    : [ 70%] Meshing curve 90 (Line)
+Info    : [ 70%] Meshing curve 91 (Circle)
+Info    : [ 70%] Meshing curve 92 (Circle)
+Info    : [ 70%] Meshing curve 93 (Circle)
+Info    : [ 70%] Meshing curve 94 (Circle)
+Info    : [ 70%] Meshing curve 95 (Line)
+Info    : [ 70%] Meshing curve 96 (Circle)
+Info    : [ 70%] Meshing curve 97 (Line)
+Info    : [ 70%] Meshing curve 98 (Circle)
+Info    : [ 70%] Meshing curve 99 (Line)
+Info    : [ 70%] Meshing curve 100 (Circle)
+Info    : [ 70%] Meshing curve 101 (Line)
+Info    : [ 80%] Meshing curve 102 (Circle)
+Info    : [ 80%] Meshing curve 103 (Line)
+Info    : [ 80%] Meshing curve 104 (Line)
+Info    : [ 80%] Meshing curve 105 (Line)
+Info    : [ 80%] Meshing curve 106 (Line)
+Info    : [ 80%] Meshing curve 107 (Line)
+Info    : [ 80%] Meshing curve 108 (Line)
+Info    : [ 80%] Meshing curve 109 (Line)
+Info    : [ 80%] Meshing curve 110 (Line)
+Info    : [ 80%] Meshing curve 111 (Line)
+Info    : [ 80%] Meshing curve 112 (Line)
+Info    : [ 80%] Meshing curve 113 (Line)
+Info    : [ 80%] Meshing curve 114 (Line)
+Info    : [ 80%] Meshing curve 115 (Circle)
+Info    : [ 80%] Meshing curve 116 (Circle)
+Info    : [ 90%] Meshing curve 117 (Circle)
+Info    : [ 90%] Meshing curve 118 (Circle)
+Info    : [ 90%] Meshing curve 119 (Line)
+Info    : [ 90%] Meshing curve 120 (Circle)
+Info    : [ 90%] Meshing curve 121 (Line)
+Info    : [ 90%] Meshing curve 122 (Circle)
+Info    : [ 90%] Meshing curve 123 (Line)
+Info    : [ 90%] Meshing curve 124 (Circle)
+Info    : [ 90%] Meshing curve 125 (Line)
+Info    : [ 90%] Meshing curve 126 (Circle)
+Info    : [ 90%] Meshing curve 127 (Circle)
+Info    : [ 90%] Meshing curve 128 (Line)
+Info    : [ 90%] Meshing curve 129 (Circle)
+Info    : [ 90%] Meshing curve 130 (Circle)
+Info    : [100%] Meshing curve 131 (Line)
+Info    : [100%] Meshing curve 132 (Circle)
+Info    : [100%] Meshing curve 133 (Circle)
+Info    : [100%] Meshing curve 134 (Line)
+Info    : [100%] Meshing curve 135 (Circle)
+Info    : [100%] Meshing curve 136 (Circle)
+Info    : [100%] Meshing curve 137 (Line)
+Info    : [100%] Meshing curve 138 (Circle)
+Info    : [100%] Meshing curve 139 (Circle)
+Info    : [100%] Meshing curve 140 (Line)
+Info    : [100%] Meshing curve 141 (Circle)
+Info    : [100%] Meshing curve 142 (Circle)
+Info    : [100%] Meshing curve 143 (Line)
+Info    : [100%] Meshing curve 144 (Circle)
+Info    : Done meshing 1D (Wall 0.0381845s, CPU 0.037851s)
+Info    : Meshing 2D...
+Info    : [  0%] Meshing surface 1 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 2 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 3 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 4 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 5 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 6 (Plane, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 7 (Cylinder, Frontal-Delaunay)
+Info    : [ 10%] Meshing surface 8 (Cylinder, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 9 (Cylinder, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 10 (Cylinder, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 11 (Cylinder, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 12 (Cylinder, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 13 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 14 (Plane, Frontal-Delaunay)
+Info    : [ 20%] Meshing surface 15 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 16 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 17 (Plane, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 18 (Cylinder, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 19 (Cylinder, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 20 (Cylinder, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 21 (Cylinder, Frontal-Delaunay)
+Info    : [ 30%] Meshing surface 22 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 23 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 24 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 25 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 26 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 27 (Plane, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 28 (Cylinder, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 29 (Cylinder, Frontal-Delaunay)
+Info    : [ 40%] Meshing surface 30 (Cylinder, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 31 (Cylinder, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 32 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 33 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 34 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 35 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 36 (Plane, Frontal-Delaunay)
+Info    : [ 50%] Meshing surface 37 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 38 (Cylinder, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 39 (Cylinder, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 40 (Cylinder, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 41 (Cylinder, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 42 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 43 (Plane, Frontal-Delaunay)
+Info    : [ 60%] Meshing surface 44 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 45 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 46 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 47 (Plane, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 48 (Cylinder, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 49 (Cylinder, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 50 (Cylinder, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 51 (Cylinder, Frontal-Delaunay)
+Info    : [ 70%] Meshing surface 52 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 53 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 54 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 55 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 56 (Cylinder, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 57 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 58 (Plane, Frontal-Delaunay)
+Info    : [ 80%] Meshing surface 59 (Cylinder, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 60 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 61 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 62 (Cylinder, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 63 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 64 (Plane, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 65 (Cylinder, Frontal-Delaunay)
+Info    : [ 90%] Meshing surface 66 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 67 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 68 (Cylinder, Frontal-Delaunay)
+Info    : [100%] Meshing surface 69 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 70 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 71 (Cylinder, Frontal-Delaunay)
+Info    : [100%] Meshing surface 72 (Plane, Frontal-Delaunay)
+Info    : [100%] Meshing surface 73 (Plane, Frontal-Delaunay)
+Info    : Done meshing 2D (Wall 0.185534s, CPU 0.182568s)
+Info    : Meshing 3D...
+Info    : 3D Meshing 7 volumes with 7 connected components
+Info    : Input mesh hash fbbf3ccbac5b78e4
+Info    : Creating an empty mesh with 4368 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of       4364 points on   1 threads - mesh.nvert: 4         
+Info    : Recovering 658 missing facet(s)
+Info    : Recover Delaunay
+Info    : Steiner(s) point(s) were inserted
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of       5197 points on   1 threads - mesh.nvert: 4369      
+Info    :           -       4894 points filtered
+Info    :           =        303 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of        549 points on   1 threads - mesh.nvert: 4672      
+Info    :           -        416 points filtered
+Info    :           =        133 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of        104 points on   1 threads - mesh.nvert: 4805      
+Info    :           -         85 points filtered
+Info    :           =         19 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of         18 points on   1 threads - mesh.nvert: 4824      
+Info    :           -         17 points filtered
+Info    :           =          1 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          1 points on   1 threads - mesh.nvert: 4825      
+Info    :           -          1 points filtered
+Info    :           =          0 points added
+Info    : Improving       3996 tet. on   1 thrd (S & ER)
+Info    : Improving       3269 tet. on   1 thrd (S & ER)
+Info    : Improving       3201 tet. on   1 thrd (S & ER)
+Info    : Improving       3181 tet. on   1 thrd (S & ER)
+Info    : Improving       3179 tet. on   1 thrd (S & ER)
+Info    : Improving       3171 tet. on   1 thrd (GSC)
+Info    : Improving       3161 tet. on   1 thrd (S & ER)
+Info    : Improving       3131 tet. on   1 thrd (S & ER)
+Info    : Improving       3107 tet. on   1 thrd (S & ER)
+Info    : Improving       3101 tet. on   1 thrd (S & ER)
+Info    : Improving       3099 tet. on   1 thrd (S & ER)
+Info    : Improving       3100 tet. on   1 thrd (S & ER)
+Info    : Improving       3099 tet. on   1 thrd (S & ER)
+Info    : Improving       3099 tet. on   1 thrd (GSC)
+Info    : Improving       3047 tet. on   1 thrd (S & ER)
+Info    : Improving       3034 tet. on   1 thrd (S & ER)
+Info    : Improving       3032 tet. on   1 thrd (S & ER)
+Info    : Improving       3031 tet. on   1 thrd (S & ER)
+Info    : Improving       3031 tet. on   1 thrd (GSC)
+Info    : Improving       3013 tet. on   1 thrd (S & ER)
+Info    : Improving       3000 tet. on   1 thrd (S & ER)
+Info    : Improving       2996 tet. on   1 thrd (S & ER)
+Info    : Improving       2994 tet. on   1 thrd (S & ER)
+Info    : Improving       2993 tet. on   1 thrd (GSC)
+Info    : Improving       2978 tet. on   1 thrd (S & ER)
+Info    : Improving       2982 tet. on   1 thrd (S & ER)
+Info    : Improving       2983 tet. on   1 thrd (S & ER)
+Info    : Improving       2982 tet. on   1 thrd (GSC)
+Info    : Improving       2982 tet. on   1 thrd (S & ER)
+Info    : Improving       2978 tet. on   1 thrd (S & ER)
+Info    : Improving       2978 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 27167 tetrahedra
+Info    :  	Final tet. mesh contains 4825 vertices
+Info    : tEmptyMesh  	 = 	    0.012
+Info    : tVerifyBnd  	 = 	    0.002
+Info    : tBndRecovery	 = 	    0.018
+Info    : tConvertMesh	 = 	    0.002
+Info    : tRefine     	 = 	    0.007
+Info    : tOptimize   	 = 	    2.861
+Info    : Input mesh hash 49b896762221e00c
+Info    : Creating an empty mesh with 81 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of         77 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of         17 points on   1 threads - mesh.nvert: 81        
+Info    :           -         13 points filtered
+Info    :           =          4 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          2 points on   1 threads - mesh.nvert: 85        
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving          5 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 444 tetrahedra
+Info    :  	Final tet. mesh contains 87 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash 265b59b7ce3d5365
+Info    : Creating an empty mesh with 83 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of         79 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of         27 points on   1 threads - mesh.nvert: 83        
+Info    :           -         24 points filtered
+Info    :           =          3 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          5 points on   1 threads - mesh.nvert: 86        
+Info    :           -          3 points filtered
+Info    :           =          2 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving          5 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 445 tetrahedra
+Info    :  	Final tet. mesh contains 88 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash 3afcaea9cb8207f4
+Info    : Creating an empty mesh with 81 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of         77 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of         17 points on   1 threads - mesh.nvert: 81        
+Info    :           -         13 points filtered
+Info    :           =          4 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          4 points on   1 threads - mesh.nvert: 85        
+Info    :           -          3 points filtered
+Info    :           =          1 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          1 points on   1 threads - mesh.nvert: 86        
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving          3 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 449 tetrahedra
+Info    :  	Final tet. mesh contains 87 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash 310c86e5aa48c6cb
+Info    : Creating an empty mesh with 83 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of         79 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of         19 points on   1 threads - mesh.nvert: 83        
+Info    :           -         16 points filtered
+Info    :           =          3 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          5 points on   1 threads - mesh.nvert: 86        
+Info    :           -          2 points filtered
+Info    :           =          3 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving          6 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 451 tetrahedra
+Info    :  	Final tet. mesh contains 89 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash ca80f0ab2aceb767
+Info    : Creating an empty mesh with 83 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of         79 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of         18 points on   1 threads - mesh.nvert: 83        
+Info    :           -         14 points filtered
+Info    :           =          4 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving          4 tet. on   1 thrd (S & ER)
+Info    :  	Final tet. mesh contains 434 tetrahedra
+Info    :  	Final tet. mesh contains 87 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Input mesh hash b28b4a540e99b1e9
+Info    : Creating an empty mesh with 83 vertices
+Info    : Initialization of tet. mesh
+Info    : Delaunay of         79 points on   1 threads - mesh.nvert: 4         
+Info    : All volumes of the BRep were found and colorized accordingly
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of         19 points on   1 threads - mesh.nvert: 83        
+Info    :           -         16 points filtered
+Info    :           =          3 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Delaunay of          5 points on   1 threads - mesh.nvert: 86        
+Info    :           -          2 points filtered
+Info    :           =          3 points added
+Info    : Computing interpolated mesh sizes...
+Info    : Done computing interpolated mesh sizes
+Info    : Improving          6 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (S & ER)
+Info    : Improving          1 tet. on   1 thrd (GSC)
+Info    :  	Final tet. mesh contains 451 tetrahedra
+Info    :  	Final tet. mesh contains 89 vertices
+Info    : tEmptyMesh  	 = 	    0.000
+Info    : tVerifyBnd  	 = 	    0.000
+Info    : tBndRecovery	 = 	    0.000 (boundary not altered)
+Info    : tConvertMesh	 = 	    0.000 (nothing to convert)
+Info    : tRefine     	 = 	    0.000
+Info    : tOptimize   	 = 	    0.000
+Info    : Done meshing 3D (Wall 2.91111s, CPU 2.9013s)
+Info    : 5351 nodes 26837 elements
+Info    : Writing '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/mesh.inp'...
+Info    : Done writing '/Users/songuijin/Documents/GitHub/Hephaestus/runs/ccx_loop_blueprint_clean_max1_claude_opus47_xhigh_jobs5_20260504/20260504_125928/evals/attempt_00/multi/046_s15_nasa_hdbk_7005_randomvib/mesh.inp'
+
+[rc=0]
+
+$ /opt/anaconda3/envs/cadquery/bin/python /Users/songuijin/Documents/GitHub/Hephaestus/scripts/ccx_eval/wire_bcs.py mesh.inp meta.json analysis_template.inp model.inp
+  NSET=NFIXED: 437 nodes
+  NSET=NALL: 5351 nodes
+  NSET=NLOAD: 5351 nodes
+wrote model.inp: 5351 nodes, NSETs=['NFIXED', 'NALL', 'NLOAD'], Eall = ['Volume1', 'Volume2', 'Volume3', 'Volume4', 'Volume5', 'Volume6', 'Volume7']
+
+[rc=0]
+
+$ /opt/homebrew/bin/ccx_2.22 model
+
+************************************************************
+
+CalculiX Version 2.22, Copyright(C) 1998-2024 Guido Dhondt
+CalculiX comes with ABSOLUTELY NO WARRANTY. This is free
+software, and you are welcome to redistribute it under
+certain conditions, see gpl.htm
+
+************************************************************
+
+You are using an executable made on Wed Feb 11 07:16:28 UTC 2026
+ Decascading the MPC's
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 14742
+ number of nonzero lower triangular matrix elements
+ 220743
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ increment 1 attempt 1 
+ increment size= 1.000000e-02
+ sum of previous increments=0.000000e+00
+ actual step time=1.000000e-02
+ actual total time=1.000000e-02
+
+ iteration 1
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ average force= 22.141023
+ time avg. forc= 22.141023
+ largest residual force= 0.000003 in node 4397 and dof 3
+ largest increment of disp= 8.891935e+01
+ largest correction to disp= 8.855422e+01 in node 4376 and dof 3
+
+ no convergence
+
+ iteration 2
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ average force= 22.141023
+ time avg. forc= 22.141023
+ largest residual force= 0.000000 in node 3780 and dof 3
+ largest increment of disp= 8.891935e+01
+ largest correction to disp= 8.919479e-10 in node 3759 and dof 3
+
+ convergence
+
+ initial energy (at start of step) = 4.146802e-27
+
+ since start of the step: 
+ external work = 5.393564e+03
+ work performed by the damping forces = 0.000000e+00
+ netto work = 5.393564e+03
+
+ actual energy: 
+ internal energy = 2.942690e+03
+ kinetic energy = 2.256572e+00
+ elastic contact energy = 0.000000e+00
+ energy lost due to friction = 0.000000e+00
+ total energy  = 2.944946e+03
+
+ energy increase = 2.944946e+03
+
+ energy balance (absolute) = -2.448617e+03 
+ energy balance (relative) = 45.398877 % 
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ increment 2 attempt 1 
+ increment size= 1.000000e-02
+ sum of previous increments=1.000000e-02
+ actual step time=2.000000e-02
+ actual total time=2.000000e-02
+
+ iteration 1
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ average force= 17.532724
+ time avg. forc= 19.836874
+ largest residual force= 0.000002 in node 4397 and dof 3
+ largest increment of disp= 7.046112e+01
+ largest correction to disp= 7.036790e+01 in node 4376 and dof 3
+
+ no convergence
+
+ iteration 2
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ average force= 17.532724
+ time avg. forc= 19.836874
+ largest residual force= 0.000000 in node 4421 and dof 3
+ largest increment of disp= 7.046112e+01
+ largest correction to disp= 7.094835e-10 in node 3759 and dof 3
+
+ convergence; the increment size is increased to 1.500000e-02
+
+ initial energy (at start of step) = 4.146802e-27
+
+ since start of the step: 
+ external work = 4.783469e+03
+ work performed by the damping forces = 0.000000e+00
+ netto work = 4.783469e+03
+
+ actual energy: 
+ internal energy = 2.314275e+03
+ kinetic energy = 5.391955e+00
+ elastic contact energy = 0.000000e+00
+ energy lost due to friction = 0.000000e+00
+ total energy  = 2.319667e+03
+
+ energy increase = 2.319667e+03
+
+ energy balance (absolute) = -2.463802e+03 
+ energy balance (relative) = 48.418866 % 
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ increment 3 attempt 1 
+ increment size= 1.500000e-02
+ sum of previous increments=2.000000e-02
+ actual step time=3.500000e-02
+ actual total time=3.500000e-02
+
+ iteration 1
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ average force= 20.503363
+ time avg. forc= 20.059037
+ largest residual force= 0.000003 in node 3743 and dof 3
+ largest increment of disp= 1.250865e+02
+ largest correction to disp= 1.250230e+02 in node 4376 and dof 3
+
+ no convergence
+
+ iteration 2
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ average force= 20.503363
+ time avg. forc= 20.059037
+ largest residual force= 0.000000 in node 3783 and dof 3
+ largest increment of disp= 1.250865e+02
+ largest correction to disp= 1.824138e-09 in node 3745 and dof 3
+
+ convergence; the increment size is increased to 2.250000e-02
+
+ the increment size exceeds the remainder of the step and is decreased to 1.500000e-02
+
+ initial energy (at start of step) = 4.146802e-27
+
+ since start of the step: 
+ external work = 5.074454e+03
+ work performed by the damping forces = 0.000000e+00
+ netto work = 5.074454e+03
+
+ actual energy: 
+ internal energy = 2.602613e+03
+ kinetic energy = 1.024362e+01
+ elastic contact energy = 0.000000e+00
+ energy lost due to friction = 0.000000e+00
+ total energy  = 2.612857e+03
+
+ energy increase = 2.612857e+03
+
+ energy balance (absolute) = -2.461597e+03 
+ energy balance (relative) = 48.420140 % 
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ increment 4 attempt 1 
+ increment size= 1.500000e-02
+ sum of previous increments=3.500000e-02
+ actual step time=5.000000e-02
+ actual total time=5.000000e-02
+
+ iteration 1
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ average force= 18.205898
+ time avg. forc= 19.595752
+ largest residual force= 0.000003 in node 4385 and dof 3
+ largest increment of disp= 9.656223e+01
+ largest correction to disp= 9.651295e+01 in node 4376 and dof 3
+
+ no convergence
+
+ iteration 2
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the energy calculation.
+
+ average force= 18.205898
+ time avg. forc= 19.595752
+ largest residual force= 0.000000 in node 3738 and dof 3
+ largest increment of disp= 9.656223e+01
+ largest correction to disp= 7.460839e-10 in node 871 and dof 3
+
+ convergence; the increment size is increased to 2.250000e-02
+
+ the increment size exceeds the remainder of the step and is decreased to 0.000000e+00
+
+ initial energy (at start of step) = 4.146802e-27
+
+ since start of the step: 
+ external work = 4.856333e+03
+ work performed by the damping forces = 0.000000e+00
+ netto work = 4.856333e+03
+
+ actual energy: 
+ internal energy = 2.382961e+03
+ kinetic energy = 1.511773e+01
+ elastic contact energy = 0.000000e+00
+ energy lost due to friction = 0.000000e+00
+ total energy  = 2.398078e+03
+
+ energy increase = 2.398078e+03
+
+ energy balance (absolute) = -2.458254e+03 
+ energy balance (relative) = 48.901463 % 
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 14742
+ number of nonzero lower triangular matrix elements
+ 220743
+
+ increment 1 attempt 1 
+ increment size= 1.000000e+00
+ sum of previous increments=0.000000e+00
+ actual step time=1.000000e+00
+ actual total time=1.050000e+00
+
+ iteration 1
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ average force= 1000.111632
+ time avg. forc= 1000.111632
+ largest residual force= 0.000000 in node 3783 and dof 2
+ largest increment of disp= 5.143199e+01
+ largest correction to disp= 5.143199e+01 in node 82 and dof 2
+
+ no convergence
+
+ iteration 2
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ average force= 1000.111632
+ time avg. forc= 1000.111632
+ largest residual force= 0.000000 in node 4381 and dof 2
+ largest increment of disp= 5.143199e+01
+ largest correction to disp= 7.368285e-10 in node 82 and dof 2
+
+ convergence
+
+ the increment size exceeds the remainder of the step and is decreased to 0.000000e+00
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 14742
+ number of nonzero lower triangular matrix elements
+ 220743
+
+ increment 1 attempt 1 
+ increment size= 1.000000e+00
+ sum of previous increments=0.000000e+00
+ actual step time=1.000000e+00
+ actual total time=2.050000e+00
+
+ iteration 1
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ average force= 1023.895372
+ time avg. forc= 1023.895372
+ largest residual force= 0.000000 in node 866 and dof 2
+ largest increment of disp= 2.153991e+00
+ largest correction to disp= 2.153991e+00 in node 4376 and dof 3
+
+ no convergence
+
+ iteration 2
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ average force= 1023.895372
+ time avg. forc= 1023.895372
+ largest residual force= 0.000000 in node 3128 and dof 2
+ largest increment of disp= 2.153991e+00
+ largest correction to disp= 3.243616e-11 in node 3745 and dof 3
+
+ convergence
+
+ the increment size exceeds the remainder of the step and is decreased to 0.000000e+00
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+
+  The numbers below are estimated upper bounds
+
+  number of:
+
+   nodes:         5351
+   elements:        15811
+   one-dimensional elements:            0
+   two-dimensional elements:            0
+   integration points per element:           27
+   degrees of freedom per node:            3
+   layers per element:            1
+
+   distributed facial loads:            0
+   distributed volumetric loads:            0
+   concentrated loads:        26755
+   single point constraints:         1311
+   multiple point constraints:            1
+   terms in all multiple point constraints:            1
+   tie constraints:            0
+   dependent nodes tied by cyclic constraints:            0
+   dependent nodes in pre-tension constraints:            0
+
+   sets:           12
+   terms in all sets:        74383
+
+   materials:            1
+   constants per material and temperature:            2
+   temperature points per material:            1
+   plastic data points per material:            0
+
+   orientations:            0
+   amplitudes:            6
+   data points in all amplitudes:            6
+   print requests:            9
+   transformations:            0
+   property cards:            0
+
+ *WARNING reading *SOLID SECTION: parameter not recognized:
+          'E_MPA':68900.0
+ *WARNING reading *SOLID SECTION. Card image:
+          *SOLIDSECTION,ELSET=EALL,MATERIAL={'NAME':'AL_6061_T6','E_MPA':68900.0,'NU':0.33,'DENSITY_KG_M3':2700.0,'FTY_MPA':276.0,'FTU_MPA':310.0}
+
+ *WARNING reading *SOLID SECTION: parameter not recognized:
+          'NU':0.33
+ *WARNING reading *SOLID SECTION. Card image:
+          *SOLIDSECTION,ELSET=EALL,MATERIAL={'NAME':'AL_6061_T6','E_MPA':68900.0,'NU':0.33,'DENSITY_KG_M3':2700.0,'FTY_MPA':276.0,'FTU_MPA':310.0}
+
+ *WARNING reading *SOLID SECTION: parameter not recognized:
+          'DENSITY_KG_M3':2700.0
+ *WARNING reading *SOLID SECTION. Card image:
+          *SOLIDSECTION,ELSET=EALL,MATERIAL={'NAME':'AL_6061_T6','E_MPA':68900.0,'NU':0.33,'DENSITY_KG_M3':2700.0,'FTY_MPA':276.0,'FTU_MPA':310.0}
+
+ *WARNING reading *SOLID SECTION: parameter not recognized:
+          'FTY_MPA':276.0
+ *WARNING reading *SOLID SECTION. Card image:
+          *SOLIDSECTION,ELSET=EALL,MATERIAL={'NAME':'AL_6061_T6','E_MPA':68900.0,'NU':0.33,'DENSITY_KG_M3':2700.0,'FTY_MPA':276.0,'FTU_MPA':310.0}
+
+ *WARNING reading *SOLID SECTION: parameter not recognized:
+          'FTU_MPA':310.0}
+ *WARNING reading *SOLID SECTION. Card image:
+          *SOLIDSECTION,ELSET=EALL,MATERIAL={'NAME':'AL_6061_T6','E_MPA':68900.0,'NU':0.33,'DENSITY_KG_M3':2700.0,'FTY_MPA':276.0,'FTU_MPA':310.0}
+
+
+ STEP            1
+
+ *INFO reading *DYNAMIC: for implicit calculations
+       the calculation of the internal energy
+       is activated.
+
+ Dynamic analysis was selected
+
+ Newton-Raphson iterative procedure is active
+
+
+ STEP            2
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+ Newton-Raphson iterative procedure is active
+
+
+ STEP            3
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+ Newton-Raphson iterative procedure is active
+
+
+ STEP            4
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+ Newton-Raphson iterative procedure is active
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 14742
+ number of nonzero lower triangular matrix elements
+ 220743
+
+ increment 1 attempt 1 
+ increment size= 1.000000e+00
+ sum of previous increments=0.000000e+00
+ actual step time=1.000000e+00
+ actual total time=3.050000e+00
+
+ iteration 1
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ average force= 1202.153221
+ time avg. forc= 1202.153221
+ largest residual force= 0.000000 in node 3783 and dof 1
+ largest increment of disp= 3.056986e+01
+ largest correction to disp= 3.056986e+01 in node 953 and dof 1
+
+ no convergence
+
+ iteration 2
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ average force= 1202.153221
+ time avg. forc= 1202.153221
+ largest residual force= 0.000000 in node 4418 and dof 2
+ largest increment of disp= 3.056986e+01
+ largest correction to disp= 4.779072e-10 in node 871 and dof 1
+
+ convergence
+
+ the increment size exceeds the remainder of the step and is decreased to 0.000000e+00
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 14742
+ number of nonzero lower triangular matrix elements
+ 220743
+
+ increment 1 attempt 1 
+ increment size= 1.000000e+00
+ sum of previous increments=0.000000e+00
+ actual step time=1.000000e+00
+ actual total time=4.050000e+00
+
+ iteration 1
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ average force= 793.492920
+ time avg. forc= 793.492920
+ largest residual force= 0.000000 in node 3721 and dof 2
+ largest increment of disp= 7.457782e+01
+ largest correction to disp= 7.457782e+01 in node 82 and dof 2
+
+ no convergence
+
+ iteration 2
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ average force= 793.492920
+ time avg. forc= 793.492920
+ largest residual force= 0.000000 in node 4386 and dof 1
+ largest increment of disp= 7.457782e+01
+ largest correction to disp= 1.068359e-09 in node 892 and dof 2
+
+ convergence
+
+ the increment size exceeds the remainder of the step and is decreased to 0.000000e+00
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Determining the structure of the matrix:
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ number of equations
+ 14742
+ number of nonzero lower triangular matrix elements
+ 220743
+
+ Using up to 1 cpu(s) for setting up the structure of the matrix.
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the symmetric stiffness/mass contributions.
+
+ Factoring the system of equations using the symmetric spooles solver
+ Using up to 1 cpu(s) for spooles.
+
+ Calculating the eigenvalues and the eigenmodes
+
+U^T*M*U=1.000000 for eigenmode 1
+U^T*M*U=1.000000 for eigenmode 2
+U^T*M*U=1.000000 for eigenmode 3
+U^T*M*U=1.000000 for eigenmode 4
+U^T*M*U=1.000000 for eigenmode 5
+U^T*M*U=1.000000 for eigenmode 6
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+ Using up to 1 cpu(s) for the stress calculation.
+
+________________________________________
+
+Total CalculiX Time: 2.720465
+________________________________________
+
+
+ STEP            5
+
+ *WARNING reading *STATIC:
+          the minimum increment    0.0000000000000000     
+          is smaller then 1.e-6 times the 
+          step time;
+          the minimum increment is changed
+          to    9.9999999999999995E-007
+          which is the minimum of the initial
+          increment time and 1.e-6 times the step time
+
+ Static analysis was selected
+
+ Newton-Raphson iterative procedure is active
+
+
+ STEP            6
+
+ Frequency analysis was selected
+
+
+ Job finished
+
+
+[rc=0]