MRM-103

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MRM-103

Part of MR-100 engine series

MRM-103D
Credit: Aerojet Redmond

Redmond Hydrazine rocket engine. In Production. Steady-state thrust 0.22 N.

Status: In Production. Thrust: 0.22 N (0.04 lbf). Unfuelled mass: 1.27 kg (2.79 lb). Specific impulse: 224 s. Burn time: 636,840 s. Height: 0.14 m (0.45 ft). Diameter: 0.14 m (0.45 ft).

Engine: 1.27 kg (2.79 lb). Restarts: 210238.

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

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