|
gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:combustionChambers
|
1
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:culturalHeritage
|
gptkb:J-2_engine
|
|
gptkbp:developedBy
|
gptkb:NASA
|
|
gptkbp:diameter
|
2.4 m
|
|
gptkbp:engineCycle
|
gas-generator cycle
|
|
gptkbp:firstTestFired
|
2011
|
|
gptkbp:intendedUse
|
gptkb:Space_Launch_System
gptkb:Ares_I
gptkb:Ares_V
|
|
gptkbp:length
|
4.3 m
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:mass
|
2,470 kg
|
|
gptkbp:oxidizer
|
5.5
|
|
gptkbp:projectCancelled
|
gptkb:Ares_I
gptkb:Ares_V
|
|
gptkbp:propulsion
|
liquid oxygen
liquid hydrogen
|
|
gptkbp:specificImpulseVacuum
|
395 seconds
448 seconds
|
|
gptkbp:status
|
development suspended
|
|
gptkbp:testLocation
|
gptkb:Stennis_Space_Center
|
|
gptkbp:thrustSeaLevel
|
1,159 kN
|
|
gptkbp:thrustVacuum
|
1,307 kN
|
|
gptkbp:usedIn
|
no operational flights
|
|
gptkbp:usedOn
|
planned for upper stage
|
|
gptkbp:bfsParent
|
gptkb:Aerojet_Rocketdyne
gptkb:Aerojet_Rocketdyne_Holdings
gptkb:Aerojet_Rocketdyne_Holdings,_Inc.
gptkb:NASA_Stennis_Space_Center
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
J-2X engine
|