Status: Developed 1998-. Date: 1998-. Thrust: 294.30 kN (66,161 lbf). Unfuelled mass: 360 kg (790 lb). Specific impulse: 348 s. Burn time: 300 s. Height: 2.10 m (6.80 ft). Diameter: 1.43 m (4.69 ft).
Engine: 360 kg (790 lb). Chamber Pressure: 161.90 bar. Thrust to Weight Ratio: 83.33.