Statements (22)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:application |
upper stage propulsion
|
gptkbp:combustionChambers |
1
|
gptkbp:countryOfOrigin |
gptkb:United_States
|
gptkbp:culturalHeritage |
gptkb:RL10_engine_family
|
gptkbp:diameter |
1.5 m
|
gptkbp:engineCycle |
expander cycle
|
gptkbp:firstFlight |
2012
|
gptkbp:gimbalRange |
7 degrees
|
https://www.w3.org/2000/01/rdf-schema#label |
RL10C
|
gptkbp:length |
2.2 m
|
gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
gptkbp:oxidizer |
liquid oxygen
|
gptkbp:propulsion |
liquid hydrogen
|
gptkbp:restartCapability |
yes
|
gptkbp:specificImpulseVacuum |
447 seconds
|
gptkbp:status |
in production
|
gptkbp:thrustVacuum |
110 kN
|
gptkbp:usedIn |
gptkb:Delta_IV_upper_stage
gptkb:Vulcan_Centaur_upper_stage |
gptkbp:bfsParent |
gptkb:Vulcan_Centaur
|
gptkbp:bfsLayer |
6
|