Q11229642: Difference between revisions
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Q11229642
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{{Page|LR-91|Classes|rocket engine used on the second stages of Titan rockets}} | {{Page|LR-91|Classes|rocket engine used on the second stages of Titan rockets|Aerojet LR-91, Aerojet LR91, LR91}} | ||
Revision as of 15:50, 17 February 2025
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
Aerojet, United States,
Persia, 1960s, Republic of Haiti, 1964, rocket engine, Ekran, Dong Fang Hong 2, Tarshish, 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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