AKA: 8D723. Status: Out of Production. Date: 1960-65. Thrust: 881.00 kN (198,056 lbf). Unfuelled mass: 576 kg (1,269 lb). Specific impulse: 301 s. Specific impulse sea level: 269 s. Burn time: 120 s. Height: 1.76 m (5.78 ft).
Chambers: 2. Engine: 576 kg (1,269 lb). Chamber Pressure: 83.30 bar. Area Ratio: 14.7. Thrust to Weight Ratio: 155.97. Oxidizer to Fuel Ratio: 2.6.