RS-25 engine

GPTKB entity

Statements (138)
Predicate Object
gptkbp:instanceOf piston engine
gptkbp:burnTime 520 seconds
gptkbp:countryOfOrigin gptkb:United_States
gptkbp:culturalHeritage gptkb:SLS_program
gptkb:Space_Shuttle_program
gptkbp:cycle staged combustion
gptkbp:designation gptkb:SSME_(Space_Shuttle_Main_Engine)
gptkbp:diameter 2.39 m
gptkbp:engineType liquid-fueled
gptkbp:engineVariants gptkb:RS-25D
gptkb:RS-25E
gptkb:RS-25F
gptkbp:firstFlight 1981
gptkbp:fuelType liquid hydrogen
gptkbp:gimbalRange 10.5 degrees
gptkbp:hasFacility gptkb:Stennis_Space_Center
gptkbp:hasModel 2012
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https://www.w3.org/2000/01/rdf-schema#label RS-25 engine
gptkbp:length 4.24 m
gptkbp:manufacturer gptkb:Aerojet_Rocketdyne
gptkb:Rocketdyne
gptkbp:maxChamberPressure 207 bar
gptkbp:notableFeature first reusable liquid-fueled engine for human spaceflight
gptkbp:numberOfEnginesOnShuttle 3
gptkbp:numberOfEnginesOnSLSCore 4
gptkbp:oxidizer liquid oxygen
gptkbp:propulsion gptkb:water
gptkbp:reusable expendable (SLS)
reusable (Space Shuttle)
gptkbp:specificImpulseVacuum 366 seconds
452 seconds
gptkbp:status in production
gptkbp:thrustSeaLevel 1,669 kN
gptkbp:thrustVacuum 1,859 kN
gptkbp:usedBy gptkb:NASA
gptkbp:usedFor human spaceflight
cargo launches
gptkbp:usedIn gptkb:Space_Launch_System
gptkb:Space_Shuttle
gptkbp:usedOn gptkb:satellite
gptkb:SLS_core_stage
gptkbp:weight 3,177 kg
gptkbp:bfsParent gptkb:Aerojet_Rocketdyne
gptkb:Stennis_Space_Center
gptkbp:bfsLayer 5