Space Shuttle program (RS-25 engines)
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
space program component
|
| gptkbp:engine |
gptkb:RS-25
|
| gptkbp:engineBurnTime |
about 8.5 minutes per launch
|
| gptkbp:engineCountPerShuttle |
3
|
| gptkbp:engineDesignation |
gptkb:SSME_(Space_Shuttle_Main_Engine)
|
| gptkbp:engineDevelopmentStart |
1970s
|
| gptkbp:engineFirstFlight |
gptkb:STS-1
|
| gptkbp:engineFuel |
liquid hydrogen
|
| gptkbp:engineGimbalRange |
±10.5 degrees
|
| gptkbp:engineLastFlight |
gptkb:STS-135
|
| gptkbp:engineMountLocation |
gptkb:Space_Shuttle_orbiter_aft_section
|
| gptkbp:engineOxidizer |
liquid oxygen
|
| gptkbp:engineReusability |
reusable
|
| gptkbp:engineRole |
main propulsion during ascent
|
| gptkbp:engineSpecificImpulse |
452 seconds (vacuum)
|
| gptkbp:engineSuccessorUse |
gptkb:Space_Launch_System_(SLS)
|
| gptkbp:engineSupplier |
gptkb:Rocketdyne
|
| gptkbp:engineThrust |
1,859 kN
|
| gptkbp:engineType |
piston engine
|
| https://www.w3.org/2000/01/rdf-schema#label |
Space Shuttle program (RS-25 engines)
|
| gptkbp:partOf |
gptkb:Space_Shuttle_program
|
| gptkbp:bfsParent |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:bfsLayer |
5
|