Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
2.39 m
|
| gptkbp:engineCycle |
staged combustion
|
| gptkbp:family |
gptkb:RS-25
|
| gptkbp:firstFlight |
not yet flown (as of 2024)
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:gimbalRange |
10.5 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
RS-25E
|
| gptkbp:intendedUse |
expendable use
|
| gptkbp:length |
4.24 m
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:predecessor |
gptkb:RS-25D
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
452 seconds
|
| gptkbp:status |
planned
|
| gptkbp:thrustVacuum |
1,859 kN
|
| gptkbp:usedIn |
gptkb:Space_Launch_System
|
| gptkbp:usedOn |
gptkb:NASA_SLS_core_stage
|
| gptkbp:bfsParent |
gptkb:RS-25_engine
|
| gptkbp:bfsLayer |
6
|