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.