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
|