|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:announced
|
2012
|
|
gptkbp:chamber_pressure
|
300 bar
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:designedBy
|
gptkb:SpaceX
|
|
gptkbp:diameter
|
1.3 m
|
|
gptkbp:engine_cycle
|
full-flow staged combustion
|
|
gptkbp:engineType
|
liquid bipropellant
|
|
gptkbp:first_static_fire
|
2016
|
|
gptkbp:firstFlight
|
2019
|
|
gptkbp:fuelType
|
liquid methane
|
|
gptkbp:gimbalRange
|
15 degrees
|
|
gptkbp:hasVersion
|
gptkb:Raptor_1
gptkb:Raptor_2
gptkb:Raptor_Vacuum
|
|
gptkbp:height
|
3.1 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Raptor rocket engine
|
|
gptkbp:manufacturer
|
gptkb:SpaceX
|
|
gptkbp:mass
|
1,600 kg
|
|
gptkbp:number_of_combustion_chambers
|
1
|
|
gptkbp:oxidizer
|
liquid oxygen
|
|
gptkbp:primaryUse
|
gptkb:SpaceX_Starship_system
|
|
gptkbp:propulsion
|
liquid methane
liquid oxygen
|
|
gptkbp:specificImpulseVacuum
|
330 s
350 s
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:Merlin_engine
|
|
gptkbp:testLocation
|
gptkb:McGregor,_Texas
|
|
gptkbp:thrustSeaLevel
|
2 MN
|
|
gptkbp:thrustVacuum
|
2.2 MN
|
|
gptkbp:used_in
|
gptkb:satellite
gptkb:Super_Heavy
|
|
gptkbp:used_in_mission
|
Starship test flights
|
|
gptkbp:usedFor
|
Mars missions
lunar missions
Earth orbital missions
reusable launch vehicles
|
|
gptkbp:bfsParent
|
gptkb:SpaceX
|
|
gptkbp:bfsLayer
|
5
|