RL10 engine

GPTKB entity

Statements (78)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:application gptkb:space_exploration
gptkb:Space_Launch_System
interplanetary missions
gptkbp:chamber_pressure 1,000 psi
gptkbp:combustion_cycle expander cycle
gptkbp:combustor_type gas-generator cycle
gptkbp:cooling_method regenerative cooling
gptkbp:cooling_system regenerative cooling
gptkbp:designed_by gptkb:Aerojet_Rocketdyne
gptkbp:development_cost gptkb:significant
gptkbp:development_start_year gptkb:1955
gptkbp:diameter 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
gptkbp:bfsLayer 4