LR-91

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Q11229642




The LR91 was an American liquid-propellant rocket engine, which was used on the second stages of Titan intercontinental ballistic missiles and launch vehicles. While the original version - the LR91-3 - ran on RP-1/LOX (as did the companion LR87-3) on the Titan I, the models that propelled the Titan II and later were switched to Aerozine 50/N2O4.

1964  Wikimedia, Wikidata
Aerojet LR-91; Aerojet LR91; LR91
rocket engine, Aerojet, 
Persia, Republic of Haiti, 1964, rocket engine, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Sikh Confederacy, United States, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz, 

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Location: KML, Cluster Map, Maps,

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