RL10-CE3

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:application gptkb:Space_Launch_System
gptkbp:check_in_time approximately 10 minutes
gptkbp:collaboration Aerojet Rocketdyne and NASA
gptkbp:combustor_type expander cycle
gptkbp:cooling_system regenerative cooling
gptkbp:debut multiple launches
gptkbp:design Aerojet Rocketdyne engineers
gptkbp:design_purpose upper stage propulsion
gptkbp:development gptkb:NASA
gptkbp:development_cost $100 million
gptkbp:engine gptkb:RL10_family
expander cycle
gptkbp:engine_configuration single engine
gptkbp:engine_type gptkb:RL10-CE
gptkb:RL10-CE2
gptkb:Team_Rocket
gptkbp:environmental_impact low emissions
gptkbp:exhaust_system aerospike nozzle
gptkbp:facilities gptkb:NASA_Marshall_Space_Flight_Center
gptkbp:first_flight gptkb:2016
gptkbp:fuel_capacity 3.5 m
1.1 m
gptkbp:fuel_economy high
gptkbp:fuel_type liquid hydrogen
gptkbp:future_plans upgraded versions
gptkbp:has_programs gptkb:NASA's_Artemis_program
https://www.w3.org/2000/01/rdf-schema#label RL10-CE3
gptkbp:inspired_by gptkb:RL10
gptkbp:is_tested_for successful
gptkbp:launch_event 100%
gptkbp:launch_vehicle gptkb:Atlas_V
gptkbp:manufacturer gptkb:Aerojet_Rocketdyne
gptkbp:material lightweight alloys
gptkbp:number_of_rooms 1,000 psi
gptkbp:operational_since gptkb:2016
gptkbp:operational_status active
gptkbp:oxidation_states liquid oxygen
gptkbp:part_of gptkb:NASA's_Space_Launch_System
gptkbp:performance meets specifications
gptkbp:propulsion 18.6
22,300 lbf
gptkbp:reliability high
gptkbp:research_and_development ongoing
gptkbp:safety_record excellent
gptkbp:specific_impulse 450 seconds
gptkbp:successor gptkb:RL10_C-1
gptkbp:used_by gptkb:United_Launch_Alliance
gptkbp:used_in Centaur upper stage
gptkbp:weight 1,200 lb
gptkbp:bfsParent gptkb:RL10_engine
gptkbp:bfsLayer 5