Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.05 m
|
| gptkbp:engineType |
gptkb:RL10
|
| gptkbp:firstFlight |
2002
|
| gptkbp:length |
12.68 m
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
active
|
| gptkbp:thrustVacuum |
99.2 kN
|
| gptkbp:usedFor |
interplanetary missions
orbital insertion payload deployment |
| gptkbp:usedOn |
gptkb:Atlas_V
|
| gptkbp:bfsParent |
gptkb:RL10_engine
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Atlas V Centaur upper stage
|