LR8-RM-5

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LR8-RM-5

Reaction Motors. Advanced version of the LR-11, 4 chambers. Engine in the X-1E was modified in 1958 to increase chamber pressure to 20 atm and burn Hydyne fuel.

Status: Out of Production. Thrust: 26.67 kN (5,996 lbf). Height: 1.45 m (4.75 ft). Diameter: 0.46 m (1.50 ft).

Chambers: 4. Thrust (sl): 26.670 kN (5,996 lbf). Thrust (sl): 2,720 kgf. Engine: 157 kg (346 lb). Chamber Pressure: 17.00 bar.

Country: USA. Spacecraft: D-558-2, X-1E. Propellants: Lox/Alcohol. Agency: Reaction Motors.

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