Space Shuttle Orbital Maneuvering System (OMS)
GPTKB entity
Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
spacecraft propulsion system
|
| gptkbp:engineType |
gptkb:AJ10-190
|
| gptkbp:firstFlight |
gptkb:STS-1
|
| gptkbp:fuelType |
4,087 kg MMH
|
| https://www.w3.org/2000/01/rdf-schema#label |
Space Shuttle Orbital Maneuvering System (OMS)
|
| gptkbp:lastFlight |
gptkb:STS-135
|
| gptkbp:locationOnShuttle |
aft fuselage pods
|
| gptkbp:manufacturer |
gptkb:Aerojet
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:operatedBy |
gptkb:NASA
|
| gptkbp:oxidizer |
nitrogen tetroxide (N2O4)
|
| gptkbp:oxidizerCapacity |
6,743 kg N2O4
|
| gptkbp:primaryUse |
orbital maneuvering
orbital insertion deorbit burn |
| gptkbp:propulsion |
monomethylhydrazine (MMH)
|
| gptkbp:specificImpulseVacuum |
316 seconds
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
26.7 kN
|
| gptkbp:totalImpulse |
1,000,000 lbf·s
|
| gptkbp:usedFor |
deorbit burns
abort to orbit scenarios orbital changes rendezvous maneuvers |
| gptkbp:usedOn |
gptkb:Space_Shuttle
|
| gptkbp:bfsParent |
gptkb:Aerojet_Rocketdyne_AJ10-190
|
| gptkbp:bfsLayer |
7
|