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RS-27C
Part of LR79 Family
RS-27A
RS-27A
Credit: Boeing / Rocketdyne
Rocke. First flight 1990.

Number: 107 . Thrust: 1,054.20 kN (236,994 lbf). Unfuelled mass: 1,091 kg (2,405 lb). Specific impulse: 302 s. Specific impulse sea level: 255 s. Burn time: 265 s. Height: 3.78 m (12.40 ft). Diameter: 2.44 m (8.00 ft).

Thrust (sl): 890.100 kN (200,102 lbf). Thrust (sl): 90,768 kgf. Engine: 1,091 kg (2,405 lb). Chamber Pressure: 48.00 bar. Area Ratio: 12. Thrust to Weight Ratio: 98.5320652356858. Oxidizer to Fuel Ratio: 2.245. Coefficient of Thrust vacuum: 1.47. Coefficient of Thrust sea level: 1.22.



Country: USA. Launch Vehicles: Barbarian MDD, Delta 7925. Propellants: Lox/Kerosene. Stages: Delta Thor XLT-C. Agency: Rocketdyne.

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