Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
expander cycle
|
| gptkbp:diameter |
1.5 m
|
| gptkbp:engineType |
cryogenic
|
| gptkbp:firstFlight |
2012
|
| https://www.w3.org/2000/01/rdf-schema#label |
RL10C-1
|
| gptkbp:length |
2.2 m
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:specificImpulseVacuum |
447 seconds
|
| gptkbp:status |
in service
|
| gptkbp:thrustVacuum |
110 kN
|
| gptkbp:usedIn |
gptkb:Centaur_upper_stage
gptkb:Delta_IV_upper_stage |
| gptkbp:bfsParent |
gptkb:RL10_(second_stage)
gptkb:Centaur_IIIB gptkb:RL-10 |
| gptkbp:bfsLayer |
7
|