Status: Design concept 1996-. Date: 1996-. Thrust: 98.00 kN (22,031 lbf). Unfuelled mass: 390 kg (850 lb). Specific impulse: 467 s. Height: 1.43 m (4.69 ft).
Chambers: 4. Engine: 390 kg (850 lb). Chamber Pressure: 83.00 bar. Thrust to Weight Ratio: 25.64. Oxidizer to Fuel Ratio: 6.