Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:burnTime |
up to 1250 seconds
|
| gptkbp:engineType |
pressure-fed
|
| gptkbp:firstFlight |
gptkb:STS-1
|
| gptkbp:fullName |
gptkb:Space_Shuttle_Orbital_Maneuvering_System
|
| gptkbp:lastFlight |
gptkb:STS-135
|
| gptkbp:locationOnShuttle |
aft fuselage pods
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:numberOfEnginesPerShuttle |
2
|
| gptkbp:oxidizer |
nitrogen tetroxide
|
| gptkbp:primaryUse |
orbital maneuvering
orbit insertion deorbit burn |
| gptkbp:propulsion |
monomethylhydrazine
|
| gptkbp:specificImpulseVacuum |
316 seconds
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
26.7 kN
|
| gptkbp:usedFor |
deorbiting
orbital changes rendezvous maneuvers |
| gptkbp:usedOn |
gptkb:Space_Shuttle
|
| gptkbp:bfsParent |
gptkb:AJ10
gptkb:Aerojet_Rocketdyne_AJ10 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Space Shuttle OMS
|