Statements (18)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:countryOfOrigin |
gptkb:United_States
|
gptkbp:diameter |
1.02 m
|
gptkbp:engineType |
expander cycle
|
gptkbp:firstFlight |
1962
|
https://www.w3.org/2000/01/rdf-schema#label |
RL10A-3
|
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 |
16,500 lbf
|
gptkbp:usedIn |
gptkb:Centaur_upper_stage
gptkb:Saturn_I_upper_stage |
gptkbp:weight |
131 kg
|
gptkbp:bfsParent |
gptkb:RL10_engine
|
gptkbp:bfsLayer |
6
|