Status: Developed -1994. Date: -1994. Thrust: 8,354.00 kN (1,878,053 lbf). Unfuelled mass: 11,703 kg (25,800 lb). Specific impulse: 337 s. Specific impulse sea level: 311 s. Height: 3.78 m (12.40 ft). Diameter: 4.00 m (13.10 ft).
Chambers: 4. Engine: 11,703 kg (25,800 lb). Chamber Pressure: 258.90 bar. Area Ratio: 36.87. Thrust to Weight Ratio: 72.79. Oxidizer to Fuel Ratio: 2.6.