Datasets:
Update launch vehicles database: 210 vehicles
Browse files- README.md +13 -35
- data/launch-vehicles.parquet +2 -2
README.md
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@@ -42,16 +42,12 @@ defined humanity's access to space. This dataset covers every orbital and suborb
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vehicle recorded in Wikidata, including historical rockets, active workhorses, and vehicles
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under development.
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Each entry includes physical dimensions (height, diameter, liftoff mass), payload capacity
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to low Earth orbit (LEO) and geostationary transfer orbit (GTO), first and last flight dates,
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number of stages, operational status, manufacturer, and country of origin.
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This enables analysis of global launch capability, rocket engineering evolution over decades,
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national space programme comparisons, and payload capacity trends across generations of vehicles.
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Sourced from Wikidata's structured knowledge base (class Q697175: space launch vehicle),
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maintained by the WikiProject Spaceflight community.
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## Schema
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| Column | Type | Description |
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| `manufacturer` | string | Manufacturer organisation |
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| `country` | string | Country of origin |
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| `height_m` | float | Total height (metres) |
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| `diameter_m` | float | Core diameter (metres) |
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| `mass_kg` | float | Liftoff mass (kg) |
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| `payload_leo_kg` | float | Payload capacity to LEO (kg) |
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| `last_flight` | string | Date of last flight if retired (YYYY-MM-DD) |
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| `num_stages` | int | Number of stages |
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| `status` | string | Operational status (active/retired/in development) |
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## Quick stats
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- **210** launch vehicles from **11** countries
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- **0** active, **0** retired
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- Tallest vehicle: Long March 10 (90.0 m)
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- Heaviest LEO payload: Delta IV Heavy (
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- Top countries: United States (99), Soviet Union (14), United Kingdom (6), Russia (5), People's Republic of China (2)
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## Usage
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ds = load_dataset("juliensimon/launch-vehicles", split="train")
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df = ds.to_pandas()
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#
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print(
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# Vehicles by first flight decade
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df["decade"] = (df["first_flight"].str[:4].astype(float) // 10 * 10).astype("Int64")
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print(df["decade"].value_counts().sort_index())
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# Height vs payload correlation
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import matplotlib.pyplot as plt
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subset = df.dropna(subset=["height_m", "payload_leo_kg"])
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plt.scatter(subset["height_m"], subset["payload_leo_kg"])
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plt.xlabel("Height (m)")
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plt.ylabel("LEO Payload (kg)")
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plt.title("Rocket Height vs Payload Capacity")
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plt.show()
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```
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## Data source
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vehicle recorded in Wikidata, including historical rockets, active workhorses, and vehicles
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under development.
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Sourced from Wikidata's structured knowledge base (class Q697175: space launch vehicle),
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maintained by the WikiProject Spaceflight community.
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> **Note:** Wikidata coverage varies — some vehicles lack physical specs or payload data.
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> Columns with <5% data coverage are automatically dropped during pipeline processing.
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## Schema
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| Column | Type | Description |
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| `manufacturer` | string | Manufacturer organisation |
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| `country` | string | Country of origin |
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| `height_m` | float | Total height (metres) |
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| `payload_leo_kg` | float | Payload capacity to LEO (kg) |
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Additional columns (diameter, mass, first_flight, etc.) appear when Wikidata coverage exceeds 5%.
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## Quick stats
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- **210** launch vehicles from **11** countries
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- **0** active, **0** retired
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- Tallest vehicle: Long March 10 (90.0 m)
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- Heaviest LEO payload: Delta IV Heavy (28,370 kg)
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- Top countries: United States (99), Soviet Union (14), United Kingdom (6), Russia (5), People's Republic of China (2)
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## Usage
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ds = load_dataset("juliensimon/launch-vehicles", split="train")
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df = ds.to_pandas()
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# List all vehicles by country
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print(df[["name", "country", "manufacturer"]].head(20))
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# Vehicles with known height
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if "height_m" in df.columns:
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tall = df.dropna(subset=["height_m"]).nlargest(10, "height_m")
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print(tall[["name", "country", "height_m"]])
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```
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## Data source
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data/launch-vehicles.parquet
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version https://git-lfs.github.com/spec/v1
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oid sha256:
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size
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version https://git-lfs.github.com/spec/v1
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oid sha256:311ce4efa3a941fa6d16a9378472ba1971942bff911a5d0ce7bc393815a7a207
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size 8743
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