Statements (24)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:countryOfOrigin |
gptkb:United_States
|
gptkbp:diameter |
5 meters
|
gptkbp:engine |
gptkb:RL10B-2
|
gptkbp:firstFlight |
2002
|
gptkbp:fuelTankMaterial |
aluminum-lithium alloy
|
gptkbp:fuelType |
liquid hydrogen
|
gptkbp:guidanceSystem |
inertial guidance
|
https://www.w3.org/2000/01/rdf-schema#label |
Delta IV upper stage
|
gptkbp:length |
12.2 meters
|
gptkbp:manufacturer |
gptkb:Boeing
gptkb:United_Launch_Alliance |
gptkbp:minimumPressure |
gptkb:helium
|
gptkbp:oxidizer |
liquid oxygen
|
gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
gptkbp:status |
active
|
gptkbp:thrust |
110 kN
|
gptkbp:usedOn |
gptkb:Delta_IV
gptkb:Delta_IV_Heavy gptkb:Delta_IV_Medium |
gptkbp:bfsParent |
gptkb:RL10_engine
gptkb:RL10 |
gptkbp:bfsLayer |
6
|