Number: 24 . Thrust: 33.70 kN (7,576 lbf). Unfuelled mass: 90 kg (198 lb). Specific impulse: 278 s. Burn time: 170 s. Diameter: 0.84 m (2.75 ft).
Engine: 90 kg (198 lb). Chamber Pressure: 7.00 bar. Area Ratio: 40. Propellant Formulation: RFNA/UDMH. Thrust to Weight Ratio: 38.1777777777778. Coefficient of Thrust vacuum: 13.7217788312386. Coefficient of Thrust sea level: 8.00749311695287.