Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
expander cycle
|
| gptkbp:diameter |
2.29 m
|
| gptkbp:firstFlight |
1998
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:gimbalRange |
4 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
Aerojet Rocketdyne RL10B-2
|
| gptkbp:length |
4.15 m
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:nozzleExtension |
deployable nozzle extension
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
464 seconds
|
| gptkbp:status |
in service
|
| gptkbp:thrustVacuum |
110 kN
|
| gptkbp:usedIn |
gptkb:Delta_IV
gptkb:Delta_III |
| gptkbp:usedOnStage |
gptkb:Delta_Cryogenic_Second_Stage_(DCSS)
|
| gptkbp:bfsParent |
gptkb:Interim_Cryogenic_Propulsion_Stage
|
| gptkbp:bfsLayer |
6
|