Status: Developed 1996-. Date: 1996-. Thrust: 442.00 kN (99,365 lbf). Unfuelled mass: 390 kg (850 lb). Specific impulse: 343 s. Specific impulse sea level: 310 s.
Engine: 390 kg (850 lb). Chamber Pressure: 176.00 bar. Thrust to Weight Ratio: 115.38. Oxidizer to Fuel Ratio: 3.4.