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Engine Model: MRM-103. Designer: Aerojet Redmond. Propellants: Hydrazine. Thrust(vac): 1.02 N (0.22 lbf). Isp: 224 sec. Burn time: 636,840 sec. Mass Engine: 1.27 kg (2.79 lb). Diameter: 0.14 m (0.45 ft). Length: 0.14 m (0.45 ft). Chambers: 1. Country: USA. Status: In Production.

Steady-state thrust 0.22 N.

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