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MRM-122
Part of MR-100 engine series Family
MRM-122
MRM-122
Credit: Aerojet Redmond
Redmond Hydrazine rocket engine. In Production. Steady-state thrust 51 N.

Status: In Production. Thrust: 142 N (31 lbf). Unfuelled mass: 1.56 kg (3.43 lb). Specific impulse: 228 s. Burn time: 2,684 s. Height: 0.25 m (0.82 ft). Diameter: 0.0470 m (0.1540 ft).

Engine: 1.56 kg (3.43 lb). Restarts: 7005.



Family: Storable liquid. Country: USA. Agency: Redmond.

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