Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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
|
| 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:Pratt_&_Whitney_RL10B-2 gptkb:RL10 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Delta IV upper stage
|