B-2C

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B-2C

Part of LR79

B2C/MA-1/MA-2
Credit: Boeing / Rocketdyne

Rocketdyne LOx/Kerosene rocket engine. Atlas Booster. Gas generator, pump-fed. Thrust and specific impulse values are at sea level. First flight 1958.

Date: 1954. Thrust: 1,374.00 kN (308,887 lbf). Specific impulse: 248 s. Specific impulse sea level: 248 s.

Thrust (sl): 1,374.000 kN (308,887 lbf). Thrust (sl): 140,110 kgf. Propellant Formulation: Lox/RP-1.

Country: USA. Launch Vehicles: Atlas A. Propellants: Lox/Kerosene. Agency: Rocketdyne.

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