|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:culturalHeritage
|
over 400 engines built
over 50 years in service
over 500 flights
|
|
gptkbp:cycle
|
expander cycle
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:fuelType
|
liquid hydrogen
|
|
gptkbp:hasFacility
|
gptkb:Stennis_Space_Center
gptkb:Santa_Susana_Field_Laboratory
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RL-10
|
|
gptkbp:length
|
2.2 m
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:notableFor
|
first rocket engine to use liquid hydrogen
first expander cycle engine
|
|
gptkbp:oxidizer
|
liquid oxygen
|
|
gptkbp:propulsion
|
gptkb:water
|
|
gptkbp:specificImpulseVacuum
|
450 seconds
|
|
gptkbp:status
|
in production
|
|
gptkbp:thrustVacuum
|
110 kN
|
|
gptkbp:usedBy
|
gptkb:Lockheed_Martin
gptkb:NASA
gptkb:US_Air_Force
gptkb:Aerojet_Rocketdyne
gptkb:Martin_Marietta
gptkb:Rocketdyne
gptkb:Boeing
gptkb:Pratt_&_Whitney
gptkb:McDonnell_Douglas
gptkb:General_Dynamics
gptkb:Convair
gptkb:United_Launch_Alliance
gptkb:ULA
Blue Origin (Vulcan Centaur)
|
|
gptkbp:usedFor
|
interplanetary missions
satellite launches
upper stage propulsion
space launch vehicles
|
|
gptkbp:usedIn
|
gptkb:Atlas_V
gptkb:Centaur_upper_stage
gptkb:Delta_Cryogenic_Second_Stage
gptkb:Orion_spacecraft_(planned)
gptkb:Space_Launch_System_(planned)
gptkb:Saturn_I
gptkb:Saturn_IB
gptkb:Vulcan_Centaur
|
|
gptkbp:variant
|
gptkb:RL10B-2
gptkb:RL10A-3
gptkb:RL10A-4
gptkb:RL10C-1
gptkb:RL10C-2
|
|
gptkbp:bfsParent
|
gptkb:Saturn_IV
|
|
gptkbp:bfsLayer
|
6
|