Status: In Production. Thrust: 25 N (5 lbf). Unfuelled mass: 0.90 kg (1.98 lb). Specific impulse: 285 s. Burn time: 25,000 s.
Engine: 0.90 kg (1.98 lb). Chamber Pressure: 8.00 bar. Area Ratio: 45. Thrust to Weight Ratio: 2.83. Oxidizer to Fuel Ratio: 1.85.