Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.05 m
|
| gptkbp:engineType |
gptkb:RL10
|
| gptkbp:firstFlight |
1962
|
| https://www.w3.org/2000/01/rdf-schema#label |
Centaur D
|
| gptkbp:length |
9 m
|
| gptkbp:manufacturer |
gptkb:Convair
|
| gptkbp:mass |
13,100 kg (dry)
52,000 kg (fully fueled) |
| gptkbp:notableMission |
gptkb:Pioneer_10
gptkb:Pioneer_11 gptkb:Surveyor_lunar_landers gptkb:Mariner_9 gptkb:Mariner_10 |
| gptkbp:numberOfEngines |
2
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Centaur_D-1A
|
| gptkbp:usedFor |
gptkb:satellite
satellite launches planetary missions upper stage |
| gptkbp:usedOn |
gptkb:Titan_IIIE
Atlas LV-3C |
| gptkbp:bfsParent |
gptkb:Atlas_SLV-3C_Centaur-D
gptkb:RL10 |
| gptkbp:bfsLayer |
6
|