Status: In Production. Thrust: 100 N (20 lbf). Unfuelled mass: 1.10 kg (2.40 lb). Specific impulse: 276 s. Burn time: 10,000 s.
Engine: 1.10 kg (2.40 lb). Chamber Pressure: 15.00 bar. Area Ratio: 43. Thrust to Weight Ratio: 9.09. Oxidizer to Fuel Ratio: 1.85.