Update launch vehicles database: 212 vehicles

README.md

@@ -53,20 +53,20 @@ This dataset is suitable for **tabular classification** tasks.
 |--------|------|-------------|--------|--------|
 | `wikidata_id` | str | Wikidata entity ID (e.g. 'Q14522') linking to https://www.wikidata.org/wiki/Q14522; use for enrichment joins with other Wikidata-sourced datasets | Q377174 | 0.0% |
 | `name` | str | Primary name of the launch vehicle (e.g. 'Saturn V', 'Falcon 9'); canonical English form as recorded in Wikidata | 2003 Alcântara VLS accident | 0.0% |
-| `manufacturer` | str | Organization that designed and built the vehicle (e.g. 'Boeing', 'SpaceX', 'Roscosmos'); null if manufacturer information is absent from Wikidata | Rockwell International | 40.8% |
-| `country` | str | Country of origin using full English name (e.g. 'United States of America', 'Russia', 'China'); reflects the operating nation at time of primary use | Iraq | 36.9% |
-| `height_m` | float64 | Total vehicle height from base to payload fairing tip, in metres; null when not recorded in Wikidata; tallest vehicles exceed 100 m (Saturn V: 110.6 m) | 25.0 | 94.2% |
-| `mass_kg` | float64 | Gross liftoff mass (fully fueled with payload) in kilograms; null when not recorded; ranges from ~10,000 kg (small launchers) to ~3,000,000 kg (Saturn V) | 48000.0 | 94.2% |
-| `payload_leo_kg` | float64 | Maximum payload mass deliverable to low Earth orbit (approx 200-2000 km altitude) in kilograms; null for vehicles whose LEO capacity is unrecorded or not applicable | 300.0 | 88.3% |
-| `first_flight` | str | Date of maiden flight in ISO 8601 format (YYYY-MM-DD); null for vehicles that never flew or where the date is unrecorded in Wikidata | 1985-10-03 | 93.2% |
+| `manufacturer` | str | Organization that designed and built the vehicle (e.g. 'Boeing', 'SpaceX', 'Roscosmos'); null if manufacturer information is absent from Wikidata | AgniKul Cosmos | 41.5% |
+| `country` | str | Country of origin using full English name (e.g. 'United States of America', 'Russia', 'China'); reflects the operating nation at time of primary use | India | 34.0% |
+| `height_m` | float64 | Total vehicle height from base to payload fairing tip, in metres; null when not recorded in Wikidata; tallest vehicles exceed 100 m (Saturn V: 110.6 m) | 25.0 | 92.9% |
+| `mass_kg` | float64 | Gross liftoff mass (fully fueled with payload) in kilograms; null when not recorded; ranges from ~10,000 kg (small launchers) to ~3,000,000 kg (Saturn V) | 48000.0 | 93.9% |
+| `payload_leo_kg` | float64 | Maximum payload mass deliverable to low Earth orbit (approx 200-2000 km altitude) in kilograms; null for vehicles whose LEO capacity is unrecorded or not applicable | 300.0 | 87.7% |
+| `first_flight` | str | Date of maiden flight in ISO 8601 format (YYYY-MM-DD); null for vehicles that never flew or where the date is unrecorded in Wikidata | 1985-10-03 | 93.9% |
 
 ## Quick stats
 
-- **206** launch vehicles from **10** countries
+- **212** launch vehicles from **12** countries
 - **0** active, **0** retired
 - Tallest vehicle: Long March 10 (90.0 m)
-- Heaviest LEO payload: Delta IV Heavy (13,810 kg)
-- Top countries: United States (100), Soviet Union (14), Russia (5), People's Republic of China (3), South Korea (2)
+- Heaviest LEO payload: Sea Dragon (498,952 kg)
+- Top countries: United States (108), Soviet Union (14), Russia (5), People's Republic of China (3), South Korea (2)
 
 ## Usage
 
@@ -141,4 +141,4 @@ Created by [Julien Simon](https://julien.org) — AI Operating Partner at Fortin
 
 ## License
 
-[CC0-1.0](https://creativecommons.org/licenses/by/4.0/)
+[CC0-1.0](https://creativecommons.org/publicdomain/zero/1.0/)

data/launch_vehicles.parquet

@@ -1,3 +1,3 @@
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