Status: Design concept 1996-. Date: 1996-. Thrust: 98.00 kN (22,031 lbf). Unfuelled mass: 370 kg (810 lb). Specific impulse: 474 s. Height: 4.18 m (13.70 ft).
Engine: 370 kg (810 lb). Chamber Pressure: 118.00 bar. Thrust to Weight Ratio: 27.02. Oxidizer to Fuel Ratio: 6.