LR-91

E136942

The LR-91 is a liquid-fueled rocket engine developed by Aerojet and used as the upper-stage propulsion system on various Titan family launch vehicles.

All labels observed (3)

Label Occurrences
LR-91 canonical 3
LR91 1
LR91-7 1

How this entity was disambiguated

Statements (49)

Predicate Object
instanceOf liquid-fueled rocket engine ⓘ
application intercontinental ballistic missile upper stage ⓘ
orbital launch missions ⓘ
burnTime approximately 150 to 180 seconds ⓘ
countryOfOrigin United States ⓘ
designFeature hypergolic propellants in later variants ⓘ
restart capability in some variants ⓘ
developer Aerojet ⓘ
linked to: Aerojet Rocketdyne
engineCycle gas-generator cycle ⓘ
era Cold War ⓘ
family Titan rocket family ⓘ
familyMemberOf Titan propulsion system family ⓘ
fuel Aerozine 50 ⓘ
RP-1 ⓘ
gimbalCapability engine gimbaling for thrust vector control ⓘ
manufacturer Aerojet ⓘ
linked to: Aerojet Rocketdyne
nozzleType fixed nozzle ⓘ
operator NASA ⓘ
United States Department of Defense ⓘ
oxidizer nitrogen tetroxide ⓘ
propellantCombination Aerozine 50 and nitrogen tetroxide ⓘ
RP-1 and liquid oxygen ⓘ
propellantFeedSystem turbopump-fed ⓘ
propellantType liquid propellant ⓘ
stageRole upper stage engine ⓘ
status retired ⓘ
successorTo earlier Titan upper-stage engines ⓘ
thrustVacuum approximately 100,000 pounds-force ⓘ
approximately 444 kilonewtons ⓘ
usedBy United States Air Force ⓘ
usedFor ballistic missiles ⓘ
space launch vehicles ⓘ
usedForLaunchOf civilian satellites ⓘ
interplanetary spacecraft ⓘ
military satellites ⓘ
usedInProgram Titan missile program ⓘ
linked to: Titan II ICBM

Titan space launch program ⓘ
usedOn Titan I ⓘ
Titan II ⓘ
linked to: Titan II GLV

Titan III ⓘ
Titan IV ⓘ
Titan family launch vehicles ⓘ
linked to: Titan rocket family
usedOnVariant Titan 34D ⓘ
linked to: Titan IIIC

Titan II GLV ⓘ
Titan IIIC ⓘ
Titan IIID ⓘ
linked to: Titan III

Titan IV-A ⓘ
linked to: Titan IV

Titan IV-B ⓘ
linked to: Titan IV
usedUntil early 2000s ⓘ

How these facts were elicited

Referenced by (5)

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

Titan II GLV → secondStageEngineType → LR91-7 ⓘ
linked to: LR-91
Titan II launch vehicle → secondStageEngineType → LR91 ⓘ
linked to: LR-91
Titan IIID → coreEngineType → LR-91 ⓘ