LR91

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LR91

Aerojet N2O4/Aerozine-50 rocket engine family. Titan Stage 2. Scaled down version of stage 1 engine featuring fixed single chamber.

Subtopics

LR91-3 Aerojet LOx/Kerosene rocket engine. Development begun 1957. Titan 1 Stage 2 major production version. Proposed for second stage of Juno V-A, Super-Jupiter in 1959. Flown 1959-1965.

LR91-7 Aerojet N2O4/Aerozine-50 rocket engine. Version used on Stage 2 of Gemini Titan 2 Launch Vehicle. Proposed for unflown Titan 3L2, Titan 3L4 boosters. First flight 1962.

LR91-5 Aerojet N2O4/Aerozine-50 rocket engine. Titan 2 ICBM Stage 2. Out of Production. Scaled down version of stage 1 engine featuring fixed single chamber. Gas generator cycle. First flight 1962.

LR91-9 Aerojet N2O4/Aerozine-50 rocket engine. Titan III B, C, D. Out of Production. Version used in earlier versions of Titan 3 upper stages. First flight 1965.

LR91-11 Aerojet N2O4/Aerozine-50 rocket engine. Out of production. Second stage engine for Titan 3 and 4. First flight 1968.

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