|
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 rocket
|
|
gptkbp:launched
|
over 200
|
|
gptkbp:length
|
12.68 m
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
gptkb:General_Dynamics
gptkb:Convair
gptkb:United_Launch_Alliance
|
|
gptkbp:material
|
gptkb:steel
|
|
gptkbp:notableFeature
|
first rocket stage to use liquid hydrogen and liquid oxygen
|
|
gptkbp:notableMission
|
gptkb:Mars_Reconnaissance_Orbiter
gptkb:Pioneer_missions
gptkb:Juno
gptkb:Mars_Science_Laboratory
gptkb:New_Horizons
gptkb:Voyager_1
gptkb:Voyager_2
gptkb:Mariner_missions
gptkb:Surveyor_lunar_landers
gptkb:Cassini–Huygens
|
|
gptkbp:predecessor
|
gptkb:Atlas-Agena
|
|
gptkbp:propulsion
|
liquid oxygen
liquid hydrogen
|
|
gptkbp:status
|
active
|
|
gptkbp:successor
|
gptkb:Centaur_V
|
|
gptkbp:thrust
|
99.2 kN
|
|
gptkbp:usedBy
|
gptkb:NASA
gptkb:US_Air_Force
gptkb:ULA
|
|
gptkbp:usedFor
|
upper stage
|
|
gptkbp:usedOn
|
gptkb:satellite
gptkb:Titan_rocket
gptkb:Vulcan_rocket
|
|
gptkbp:website
|
https://www.ulalaunch.com/rockets/centaur
|
|
gptkbp:bfsParent
|
gptkb:Krafft_A._Ehricke
|
|
gptkbp:bfsLayer
|
7
|