MR-120 (original) (raw)

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MR-120

Part of MR-100 engine series

MR-120
Credit: Aerojet Redmond

Redmond Hydrazine rocket engine. Small ICBM. In Production. Developed as an attitude control thruster for the small ICBM.

Status: In Production. Thrust: 90 N (20 lbf). Unfuelled mass: 0.41 kg (0.90 lb). Specific impulse: 229 s. Burn time: 150 s. Height: 0.15 m (0.49 ft). Diameter: 0.0420 m (0.1370 ft).

Engine: 0.41 kg (0.90 lb). Chamber Pressure: 12.40 bar. Area Ratio: 15. Restarts: 1911.

Family: Storable liquid. Country: USA. Launch Vehicles: SICBM. Agency: Redmond.

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