gptkbp:instance_of
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gptkb:Team_Rocket
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gptkbp:application
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gptkb:space_exploration
gptkb:Space_Launch_System
interplanetary missions
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gptkbp:chamber_pressure
|
1,000 psi
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gptkbp:combustion_cycle
|
expander cycle
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gptkbp:combustor_type
|
gas-generator cycle
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gptkbp:cooling_method
|
regenerative cooling
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gptkbp:cooling_system
|
regenerative cooling
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gptkbp:designed_by
|
gptkb:Aerojet_Rocketdyne
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gptkbp:development_cost
|
gptkb:significant
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gptkbp:development_start_year
|
gptkb:1955
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gptkbp:diameter
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1.1 meters
4.5 ft
|
gptkbp:first_flight
|
gptkb:1962
gptkb:1963
gptkb:2023
|
gptkbp:flight_style
|
over 200
|
gptkbp:fuel_type
|
liquid hydrogen
|
gptkbp:has_historical_building
|
gptkb:RL10-A
gptkb:RL10-AL
gptkb:RL10-AX
gptkb:RL10-B
gptkb:RL10-C
gptkb:RL10-CE
gptkb:RL10-CE2
gptkb:RL10-CE3
gptkb:RL10-CE4
gptkb:RL10-CE5
gptkb:RL10-CE6
gptkb:RL10-CE7
gptkb:RL10-CL
gptkb:RL10-CE8
RL10-CE10
RL10-CE11
RL10-CE12
RL10-CE13
RL10-CE14
RL10-CE15
RL10-CE16
RL10-CE17
RL10-CE18
RL10-CE19
RL10-CE20
RL10-CE9
|
https://www.w3.org/2000/01/rdf-schema#label
|
RL10 engine
|
gptkbp:length
|
15 ft
3.1 meters
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
gptkbp:notable_feature
|
high efficiency
|
gptkbp:notable_launches
|
gptkb:New_Horizons
gptkb:Mars_Reconnaissance_Orbiter
gptkb:Juno_spacecraft
gptkb:Parker_Solar_Probe
gptkb:Lunar_Reconnaissance_Orbiter
gptkb:Voyager_spacecraft
gptkb:GPS_satellites
HST (Hubble Space Telescope)
|
gptkbp:nozzle_type
|
bell nozzle
|
gptkbp:number_of_rooms
|
gptkb:1
1,000 psi
|
gptkbp:number_of_versions
|
multiple
|
gptkbp:operational_status
|
in use
|
gptkbp:oxidation_states
|
liquid oxygen
|
gptkbp:propulsion
|
22,000 lbf
22,300 lbf
|
gptkbp:specific_impulse
|
450 seconds
|
gptkbp:status
|
in service
|
gptkbp:success_rate
|
high
|
gptkbp:used_in
|
gptkb:Atlas_V_upper_stage
gptkb:Delta_IV_upper_stage
Centaur upper stage
|
gptkbp:weight
|
1,200 lb
272 kg
|
gptkbp:bfsParent
|
gptkb:Aerojet_Rocketdyne
gptkb:NASA_Stennis_Space_Center
gptkb:Rocketdyne
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gptkbp:bfsLayer
|
4
|