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LR30
Reaction Motors LOx/Ammonia rocket engine. D-558-3. Capable rocket engine planned for use in D-558-3 and X-15. Cancelled in favor of XLR-99.

AKA: XLR30-RM-2. Date: 1952-1957. Thrust: 222.60 kN (50,042 lbf).



Country: USA. Spacecraft: D-558-3. Propellants: Lox/Ammonia. Agency: Reaction Motors.

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