Space Launch System (SLS) engines
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:culturalHeritage |
Space Shuttle Main Engine (SSME)
|
| gptkbp:engineCycle |
staged combustion
|
| gptkbp:engineType |
liquid-fueled
|
| gptkbp:firstFlight |
gptkb:2022_(Artemis_I)
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:gimbalRange |
+/- 8.5 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
Space Launch System (SLS) engines
|
| gptkbp:mainEngineModel |
gptkb:RS-25
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:numberPerCoreStage |
4
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:reusable |
partially reusable
|
| gptkbp:status |
active
|
| gptkbp:thrust |
1,859 kN (RS-25)
|
| gptkbp:usedIn |
gptkb:Space_Launch_System
gptkb:Artemis_program |
| gptkbp:usedOn |
gptkb:Space_Shuttle
|
| gptkbp:bfsParent |
gptkb:Aerojet_Rocketdyne_Holdings,_Inc.
|
| gptkbp:bfsLayer |
7
|