|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:average_temperature
|
-423 to 1,500 ° F
|
|
gptkbp:check_in_time
|
8.5 minutes
|
|
gptkbp:control_system
|
digital
|
|
gptkbp:debut
|
gptkb:1976
|
|
gptkbp:designed_by
|
gptkb:Rocketdyne
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
5.5 ft
|
|
gptkbp:durability
|
gptkb:true
up to 100 flights
|
|
gptkbp:engine
|
modular
staged combustion
|
|
gptkbp:engine_configuration
|
vertical
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:first_flight
|
gptkb:1981
gptkb:2011
|
|
gptkbp:fuel_type
|
liquid hydrogen
turbopump
|
|
gptkbp:has_programs
|
gptkb:Space_Shuttle
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RS-25 N
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:length
|
14.5 ft
|
|
gptkbp:mission
|
gptkb:STS_missions
|
|
gptkbp:number_of_engines
|
four
|
|
gptkbp:number_of_rooms
|
gptkb:single
3,000 psi
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
gimbaled
190,000 lbf
63:1
|
|
gptkbp:replaced_by
|
gptkb:RS-25_D
|
|
gptkbp:specific_impulse
|
452 seconds
|
|
gptkbp:successor
|
gptkb:RS-25_E
|
|
gptkbp:total_engines_built
|
gptkb:16
|
|
gptkbp:used_in
|
gptkb:SLS_(Space_Launch_System)
gptkb:Space_Shuttle
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Rocketdyne_RS-25
|
|
gptkbp:bfsLayer
|
5
|