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Engine Model: Aerojet 2. Designer: Aerojet. Propellants: N2O4/MMH. Thrust(vac): 2.00 N (0.40 lbf). Isp: 265 sec. Mass Engine: 0.27 kg (0.59 lb). Chambers: 1. Area Ratio: 150.00. Thrust to Weight Ratio: 0.75. Country: USA. Status: In Production.

Mixture Ratio(O/F): 1.65.

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