|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:CEOOfManufacturer
|
gptkb:Elon_Musk
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:criteria
|
gptkb:NASA_Artemis_program
|
|
gptkbp:designedFor
|
Mars missions
Earth-to-Earth transport
Moon missions
|
|
gptkbp:diameter
|
9 m
|
|
gptkbp:engineArrangement
|
3 sea-level, 3 vacuum optimized
|
|
gptkbp:engineType
|
gptkb:bird
|
|
gptkbp:firstFlight
|
2023-04-20
|
|
gptkbp:height
|
50 m
|
|
gptkbp:launchSite
|
gptkb:Starbase,_Boca_Chica,_Texas
|
|
gptkbp:manufacturer
|
gptkb:SpaceX
|
|
gptkbp:mass
|
120,000 kg (dry)
1,200,000 kg (fully fueled)
|
|
gptkbp:numberOfEngines
|
6
|
|
gptkbp:partOf
|
gptkb:SpaceX_Starship_launch_system
|
|
gptkbp:payloadCapacityToMars
|
100 metric tons
|
|
gptkbp:payloadToLEO
|
100–150 metric tons
|
|
gptkbp:propulsion
|
liquid methane
liquid oxygen
|
|
gptkbp:purpose
|
cargo transport
human spaceflight
interplanetary transport
orbital launch
|
|
gptkbp:reusable
|
fully reusable
|
|
gptkbp:seatingCapacity
|
up to 100
|
|
gptkbp:status
|
in development
|
|
gptkbp:successor
|
gptkb:SpaceX_Dragon_2
|
|
gptkbp:testFlights
|
gptkb:Starship_SN10
gptkb:Starship_SN15
gptkb:Starship_SN20
gptkb:Starship_SN8
gptkb:Starship_SN9
gptkb:Starship_24
gptkb:Starship_25
gptkb:Starship_28
gptkb:Starship_29
|
|
gptkbp:upperStageOf
|
gptkb:SpaceX_Starship_launch_system
|
|
gptkbp:variant
|
gptkb:Starship_HLS
gptkb:Starship_Cargo
gptkb:Starship_Crew
gptkb:Starship_Tanker
|
|
gptkbp:website
|
https://www.spacex.com/vehicles/starship/
|
|
gptkbp:bfsParent
|
gptkb:SpaceX_Starship_development
gptkb:SpaceX_Starship_development_program
gptkb:SpaceX_Starship_launch_system
gptkb:Starship_launch_system
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Starship spacecraft
|