|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:NASA_missions
|
|
gptkbp:certification
|
NASA certified
|
|
gptkbp:combustor_type
|
3,300 ° F
|
|
gptkbp:control_system
|
digital
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut
|
gptkb:1980
|
|
gptkbp:designed_by
|
gptkb:Rocketdyne
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:durability
|
gptkb:true
|
|
gptkbp:engine
|
gptkb:RS-25_D
gptkb:NASA_Michoud_Assembly_Facility
staged combustion
first reusable rocket engine
used in SLS
|
|
gptkbp:engine_configuration
|
vertical
Rocketdyne engineers
up to 230,000 lbf
|
|
gptkbp:engine_design_life
|
100 flights
|
|
gptkbp:engine_development_program
|
gptkb:Space_Shuttle
|
|
gptkbp:engine_future_use
|
gptkb:Artemis_missions
|
|
gptkbp:engine_launch_history
|
over 135 launches
|
|
gptkbp:engine_nozzle_expansion_ratio
|
60:1
|
|
gptkbp:engine_nozzle_type
|
converging-diverging
|
|
gptkbp:engine_power
|
high
optimized for reusability
|
|
gptkbp:engine_refurbishment
|
gptkb:true
|
|
gptkbp:engine_retirement_date
|
gptkb:2011
|
|
gptkbp:engine_testing_duration
|
up to 500 seconds
|
|
gptkbp:engine_testing_milestones
|
multiple successful static fires
|
|
gptkbp:engine_thrust_chamber
|
single combustion chamber
|
|
gptkbp:engine_thrust_vector_control
|
yes
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:first_flight
|
gptkb:1981
|
|
gptkbp:fuel_capacity
|
7.5 ft
14.5 ft
|
|
gptkbp:fuel_type
|
liquid hydrogen
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RS-25 L
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:is_tested_for
|
gptkb:Stennis_Space_Center
|
|
gptkbp:number_of_engines
|
four
|
|
gptkbp:number_of_rooms
|
1,000 psi
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_period
|
over 30 years
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
190,000 lbf
63:1
|
|
gptkbp:specific_impulse
|
452 seconds
|
|
gptkbp:successor
|
gptkb:RS-25_E
|
|
gptkbp:total_engines_built
|
gptkb:16
|
|
gptkbp:used_in
|
gptkb:Space_Shuttle
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Rocketdyne_RS-25
|
|
gptkbp:bfsLayer
|
5
|