Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
2.29 m
|
| gptkbp:engineType |
expander cycle
|
| gptkbp:firstFlight |
1998
|
| https://www.w3.org/2000/01/rdf-schema#label |
RL10B-2
|
| gptkbp:length |
4.0 m
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:nozzleExtension |
deployable carbon-carbon nozzle extension
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:specificImpulseVacuum |
464 seconds
|
| gptkbp:status |
in service
|
| gptkbp:thrustVacuum |
110 kN
|
| gptkbp:usedIn |
gptkb:Delta_IV
gptkb:Delta_III gptkb:Delta_II |
| gptkbp:bfsParent |
gptkb:RL10_engine
gptkb:Delta_IV_Medium+_(4,2) gptkb:Delta_IV_Medium+_(5,2) gptkb:Delta_IV_Medium+_(5,4) gptkb:Delta_IV_Heavy gptkb:Delta_IV_Medium gptkb:Boeing_Delta_IV_Heavy |
| gptkbp:bfsLayer |
6
|