|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:developedBy
|
gptkb:NASA
|
|
gptkbp:diameter
|
3.05 m (Centaur III)
|
|
gptkbp:engineType
|
gptkb:RL10
|
|
gptkbp:firstFlight
|
1962
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Centaur upper stage
|
|
gptkbp:launchVehicle
|
gptkb:Atlas_V
gptkb:Titan_IIIE
gptkb:Atlas-Centaur
gptkb:Vulcan_Centaur
|
|
gptkbp:length
|
12.68 m (Centaur III)
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
gptkb:General_Dynamics
gptkb:Convair
gptkb:United_Launch_Alliance
|
|
gptkbp:mass
|
2,243 kg (Centaur III)
|
|
gptkbp:notableFeature
|
first rocket stage to use liquid hydrogen and liquid oxygen
restartable engine
thin stainless steel balloon tanks
|
|
gptkbp:notableMission
|
gptkb:Mars_Reconnaissance_Orbiter
gptkb:Juno
gptkb:Mars_Science_Laboratory
gptkb:New_Horizons
gptkb:Pioneer_10
gptkb:Pioneer_11
gptkb:Surveyor_lunar_landers
|
|
gptkbp:propulsion
|
liquid oxygen
liquid hydrogen
|
|
gptkbp:status
|
active
|
|
gptkbp:successor
|
gptkb:ACES_upper_stage
gptkb:Vulcan_Centaur
|
|
gptkbp:usedFor
|
interplanetary missions
geostationary transfer orbit
Earth orbit insertion
|
|
gptkbp:usedOn
|
gptkb:Atlas_V
gptkb:Atlas_I
gptkb:Titan_IIIE-Centaur
gptkb:satellite
gptkb:Atlas_III
gptkb:Atlas_G
gptkb:Atlas_V_551
gptkb:Atlas_V_401
gptkb:Titan_rocket
gptkb:Atlas-Centaur
gptkb:Vulcan_rocket
gptkb:Atlas_II
gptkb:Vulcan_Centaur
|
|
gptkbp:bfsParent
|
gptkb:Agena_upper_stage
|
|
gptkbp:bfsLayer
|
5
|