Status: Study 1959. Thrust: 355.70 kN (79,965 lbf). Unfuelled mass: 1,438 kg (3,170 lb). Specific impulse: 425 s. Specific impulse sea level: 306 s. Burn time: 656 s.
Thrust (sl): 256.100 kN (57,574 lbf). Thrust (sl): 26,117 kgf. Engine: 1,438 kg (3,170 lb). Chamber Pressure: 30.00 bar. Area Ratio: 28. Thrust to Weight Ratio: 25.22.