Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.02 m
|
| gptkbp:engineType |
expander cycle
|
| gptkbp:firstFlight |
1962
|
| gptkbp:length |
2.29 m
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:specificImpulseVacuum |
451 seconds
|
| gptkbp:status |
retired
|
| gptkbp:thrustVacuum |
110 kN
|
| gptkbp:usedFor |
upper stage propulsion
|
| gptkbp:usedIn |
gptkb:Centaur_upper_stage
gptkb:Saturn_I_upper_stage |
| gptkbp:weight |
131 kg
|
| gptkbp:bfsParent |
gptkb:RL10_engine
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
RL10A-4-2
|