Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:burnTime |
up to 800 seconds
|
| 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 rocket stage
|
| gptkbp:length |
12.68 m
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
gptkb:General_Dynamics gptkb:Convair |
| gptkbp:notableFor |
first rocket stage to use liquid hydrogen and liquid oxygen
|
| gptkbp:predecessor |
gptkb:Atlas_Able_upper_stage
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
active
|
| gptkbp:successor |
gptkb:Centaur_V
|
| gptkbp:thrust |
gptkb:99.2_kN_(RL10A-4-2)
|
| gptkbp:usedFor |
upper stage
|
| gptkbp:usedIn |
planetary missions
Earth orbit missions |
| gptkbp:usedOn |
gptkb:Atlas_V
gptkb:Titan_IIIE gptkb:Atlas-Centaur gptkb:Vulcan_Centaur |
| gptkbp:website |
https://www.ulalaunch.com/rockets/centaur
|
| gptkbp:bfsParent |
gptkb:Consolidated_Vultee_Aircraft
gptkb:Consolidated_Vultee_Aircraft_Corporation |
| gptkbp:bfsLayer |
7
|