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gptkbp:instanceOf
|
spacecraft stage
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|
gptkbp:alsoKnownAs
|
gptkb:Starship_upper_stage
|
|
gptkbp:armament
|
tiled heat shield
|
|
gptkbp:cargoVariant
|
gptkb:Starship_Cargo
|
|
gptkbp:crewVersion
|
gptkb:Starship_Crew
|
|
gptkbp:designedFor
|
Mars missions
lunar missions
point-to-point Earth transport
orbital flight
|
|
gptkbp:diameter
|
9 meters
|
|
gptkbp:engineArrangement
|
3 sea-level, 3 vacuum Raptor engines
|
|
gptkbp:engineType
|
methalox
|
|
gptkbp:firstFlight
|
April 20, 2023
|
|
gptkbp:firstIntegratedFlight
|
April 20, 2023
|
|
gptkbp:fuelType
|
liquid methane
|
|
gptkbp:guidanceSystem
|
autonomous
|
|
gptkbp:heatShieldMaterial
|
hexagonal ceramic tiles
|
|
gptkbp:height
|
50 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Starship second stage
|
|
gptkbp:landingCapability
|
vertical landing
|
|
gptkbp:landingLegs
|
integrated into body flaps
|
|
gptkbp:launchSite
|
gptkb:Starbase,_Texas
|
|
gptkbp:manufacturer
|
gptkb:SpaceX
|
|
gptkbp:mass
|
~120,000 kg
|
|
gptkbp:material
|
gptkb:steel
|
|
gptkbp:minimumPressure
|
autogenous
|
|
gptkbp:notableTestFlight
|
March 14, 2024
June 6, 2024
November 18, 2023
|
|
gptkbp:numberOfEngines
|
6
|
|
gptkbp:operator
|
gptkb:SpaceX
|
|
gptkbp:oxidizer
|
liquid oxygen
|
|
gptkbp:partOf
|
gptkb:SpaceX_Starship_launch_system
|
|
gptkbp:payloadCapacityToMars
|
~100 metric tons
|
|
gptkbp:payloadToLEO
|
~100-150 metric tons
|
|
gptkbp:primaryPropulsion
|
gptkb:Raptor_engines
|
|
gptkbp:propellantCapacity
|
~1,200,000 kg
|
|
gptkbp:reusable
|
true
|
|
gptkbp:seatingCapacity
|
up to 100
|
|
gptkbp:status
|
in development
|
|
gptkbp:successor
|
gptkb:Falcon_9_upper_stage
gptkb:Falcon_Heavy_upper_stage
|
|
gptkbp:testFlights
|
multiple
|
|
gptkbp:usedFor
|
gptkb:NASA_Artemis_program_(lunar_lander_variant)
human spaceflight
interplanetary missions
satellite launches
Starlink deployment
|
|
gptkbp:bfsParent
|
gptkb:Raptor_Vacuum
|
|
gptkbp:bfsLayer
|
7
|