|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:cycle
|
expander cycle
|
|
gptkbp:diameter
|
1.0 m
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:gimbalRange
|
4 degrees
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RL10 rocket engine
|
|
gptkbp:length
|
2.2 m
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:mass
|
277 kg
|
|
gptkbp:notableFor
|
first rocket engine to use liquid hydrogen
|
|
gptkbp:numberBuilt
|
over 500
|
|
gptkbp:predecessor
|
none
|
|
gptkbp:propulsion
|
liquid oxygen
liquid hydrogen
|
|
gptkbp:restartable
|
yes
|
|
gptkbp:specificImpulseVacuum
|
450 seconds
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:RL10C
|
|
gptkbp:thrustVacuum
|
110 kN
|
|
gptkbp:usedIn
|
gptkb:Atlas_V
gptkb:Delta_IV
gptkb:Dragon
gptkb:Space_Launch_System
gptkb:Centaur_upper_stage
gptkb:Delta_IV_upper_stage
gptkb:Dream_Chaser
gptkb:Vulcan_Centaur_upper_stage
gptkb:Atlas_V_upper_stage
gptkb:Orion_spacecraft_(planned)
gptkb:Saturn_IB_upper_stage
gptkb:Space_Launch_System_(planned)
gptkb:Titan_III_upper_stage
gptkb:X-33_(planned)
gptkb:Orion_spacecraft
gptkb:Saturn_I
gptkb:Saturn_IB
gptkb:Saturn_I_upper_stage
gptkb:Dream_Chaser_(planned)
gptkb:X-33
gptkb:Titan_III
gptkb:Vulcan_Centaur
gptkb:DC-XA
|
|
gptkbp:usedOn
|
NASA missions
US Air Force missions
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_Rocketdyne
|
|
gptkbp:bfsLayer
|
6
|