Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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
|
| 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 |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
RL10C
|