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Aerojet General LR-87-5

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Two chamber liquid fueled engine uses an oxidizer that could be stored in missile for long periods of time. Engines could not be throttled or restarted after launch if shutdown. Powers the first stage of a 2 stage missile.

Technical Specifications
Rated Output 430,000 lbs thrust
Commonly Used On LGM-25C Titan II, Titan III, Titan 34D, & Titan IV


Location: Titan Missile Museum