Status: Developed 1980's. Thrust: 8.00 N (1.70 lbf). Unfuelled mass: 0.0250 kg (0.0550 lb). Specific impulse: 296 s.
Engine: 0.0250 kg (0.0550 lb). Chamber Pressure: 30.00 bar. Thrust to Weight Ratio: 32.79.