|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:Space_Launch_System
space launch vehicles
|
|
gptkbp:average_temperature
|
-423 ° F to 1,500 ° F
|
|
gptkbp:chamber_pressure
|
1,000 psi
|
|
gptkbp:combustion_cycle
|
gas-generator cycle
expander cycle
|
|
gptkbp:control_system
|
electronic control
|
|
gptkbp:cooling_method
|
regenerative cooling
radiative cooling
|
|
gptkbp:development
|
gptkb:NASA_Marshall_Space_Flight_Center
gptkb:NASA
|
|
gptkbp:development_cost
|
gptkb:significant
|
|
gptkbp:diameter
|
4.5 ft
|
|
gptkbp:engine_cycle
|
expander cycle
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:flight_style
|
over 200
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
liquid hydrogen
|
|
gptkbp:has_historical_building
|
gptkb:RL10_C-1
gptkb:RL10_A-3
gptkb:RL10_B-1
gptkb:RL10_C-3
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RL10 rocket engine
|
|
gptkbp:ignition_system
|
pyrotechnic
|
|
gptkbp:launch_vehicle
|
gptkb:Centaur
gptkb:Delta_IV
gptkb:Ariane_5
gptkb:Vulcan_Centaur
gptkb:Space_Launch_System
gptkb:Titan_IV
gptkb:Atlas_II
gptkb:Titan_III
gptkb:Space_Launch_System_(SLS)
gptkb:Delta_II
gptkb:Atlas_V
|
|
gptkbp:length
|
12 ft
15 ft
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:notable_mission
|
gptkb:New_Horizons_mission
gptkb:Juno_mission
gptkb:Voyager_program
gptkb:Mars_missions
Lunar missions
Commercial crew missions
Hubble Space Telescope launch
International Space Station resupply missions
GPS satellite launches
Parker Solar Probe launch
Iridium satellite launches
|
|
gptkbp:notable_users
|
gptkb:Lockheed_Martin
gptkb:United_Launch_Alliance
gptkb:Boeing
gptkb:NASA
|
|
gptkbp:nozzle_type
|
bell nozzle
|
|
gptkbp:number_of_chambers
|
gptkb:1
|
|
gptkbp:number_of_variants
|
multiple
|
|
gptkbp:operational_since
|
gptkb:1963
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
18:1
22,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:specific_impulse
|
450 seconds
|
|
gptkbp:status
|
in production
|
|
gptkbp:testing_facility
|
gptkb:NASA_Marshall_Space_Flight_Center
Aerojet Rocketdyne facility
|
|
gptkbp:used_by
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:United_Launch_Alliance
gptkb:NASA
|
|
gptkbp:used_in
|
gptkb:Atlas_V_upper_stage
gptkb:Delta_IV_upper_stage
Centaur upper stage
|
|
gptkbp:variant
|
gptkb:RL10_C-1
gptkb:RL10_A-3
gptkb:RL10_B-2
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Aerojet_Rocketdyne_Propulsion
|
|
gptkbp:bfsLayer
|
5
|