|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:combustionChambers
|
~300 bar
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:cycle
|
full-flow staged combustion
|
|
gptkbp:designedBy
|
gptkb:SpaceX_Propulsion_Team
|
|
gptkbp:diameter
|
1.3 meters
|
|
gptkbp:engineDesignation
|
gptkb:Raptor_SL
gptkb:Raptor_Vac
|
|
gptkbp:engineMaterial
|
gptkb:steel
gptkb:Inconel
|
|
gptkbp:engineType
|
full-flow staged combustion
|
|
gptkbp:engineVariants
|
sea-level
vacuum optimized
|
|
gptkbp:firstFlight
|
2016
|
|
gptkbp:fuelType
|
methane
|
|
gptkbp:gimbalRange
|
15 degrees
|
|
gptkbp:hasFacility
|
gptkb:SpaceX_Boca_Chica
gptkb:SpaceX_McGregor
|
|
gptkbp:hasVersion
|
gptkb:Raptor_1
gptkb:Raptor_2
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SpaceX Raptor
|
|
gptkbp:length
|
3.1 meters
|
|
gptkbp:manufacturer
|
gptkb:SpaceX
|
|
gptkbp:notableFeature
|
full-flow staged combustion cycle
methalox propellant
high reusability
|
|
gptkbp:numberOfEnginesOnStarship
|
6
|
|
gptkbp:numberOfEnginesOnSuperHeavy
|
33
|
|
gptkbp:oxidizer
|
liquid oxygen
|
|
gptkbp:primaryUse
|
gptkb:Starship_launch_system
|
|
gptkbp:propulsion
|
liquid methane
liquid oxygen
|
|
gptkbp:reusable
|
yes
|
|
gptkbp:specificImpulseVacuum
|
~330 seconds
~380 seconds
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:SpaceX_Merlin
|
|
gptkbp:thrustSeaLevel
|
~185 metric tons
|
|
gptkbp:thrustVacuum
|
~230 metric tons
|
|
gptkbp:usedFor
|
orbital launches
Mars missions
lunar missions
|
|
gptkbp:usedIn
|
gptkb:satellite
gptkb:Super_Heavy
|
|
gptkbp:usedOn
|
gptkb:Super_Heavy_booster
gptkb:Starship_upper_stage
|
|
gptkbp:bfsParent
|
gptkb:bird
|
|
gptkbp:bfsLayer
|
4
|