AJ10-190

E837364

The AJ10-190 is a hypergolic rocket engine used on NASA’s Space Shuttle Orbital Maneuvering System for in-space propulsion and orbital adjustments.

All labels observed (1)

Label Occurrences
AJ10-190 canonical 2

How this entity was disambiguated

Statements (45)

Predicate Object
instanceOf hypergolic rocket engine ⓘ
liquid-propellant rocket engine ⓘ
rocket engine ⓘ
application deorbit burn ⓘ
in-space propulsion ⓘ
orbit adjustment ⓘ
orbit circularization ⓘ
orbital maneuvering ⓘ
associatedSpacecraft Space Shuttle Atlantis ⓘ
Space Shuttle Challenger ⓘ
Space Shuttle Columbia ⓘ
Space Shuttle Discovery ⓘ
Space Shuttle Endeavour ⓘ
coolingMethod film cooling ⓘ
countryOfOrigin United States ⓘ
cycleType pressure-fed cycle ⓘ
designedFor human-rated spacecraft ⓘ
firstFlightProgram STS-1 ⓘ
firstFlightVehicle Space Shuttle Columbia ⓘ
firstFlightYear 1981 ⓘ
fuel monomethylhydrazine ⓘ
gimbalCapability gimballed for thrust vector control ⓘ
heritage Aerojet AJ10 engine family ⓘ
ignitionSystem hypergolic ignition ⓘ
manufacturer Aerojet ⓘ
linked to: Aerojet Rocketdyne
mountingLocation aft fuselage of Space Shuttle orbiter ⓘ
operatedIn vacuum of space ⓘ
oxidizer dinitrogen tetroxide ⓘ
partOf Space Shuttle Orbital Maneuvering System engine pod ⓘ
propellantType hypergolic ⓘ
restartCapability multiple restart ⓘ
shutdownMethod propellant flow cutoff ⓘ
specificImpulseVacuum about 316 seconds ⓘ
status retired ⓘ
throttleCapability fixed thrust ⓘ
thrustVacuum about 26.7 kilonewtons ⓘ
about 6,000 pounds-force ⓘ
usedBy NASA ⓘ
usedDuringProgram Space Shuttle program ⓘ
usedFor deorbit maneuvers ⓘ
orbital insertion burns ⓘ
plane change maneuvers ⓘ
rendezvous maneuvers ⓘ
usedOn Space Shuttle Orbital Maneuvering System ⓘ
Space Shuttle orbiter ⓘ

How these facts were elicited

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.