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LR105-3
Part of LR105 Family
Rocketdyne LOx/Kerosene rocket engine. Out of Production. Early version of Atlas Sustainer. Gas generator, pump-fed.

Status: Out of Production. Thrust: 375.00 kN (84,303 lbf). Specific impulse: 308 s. Specific impulse sea level: 220 s.

Thrust (sl): 267.000 kN (60,023 lbf). Thrust (sl): 27,200 kgf. Chamber Pressure: 50.30 bar. Oxidizer to Fuel Ratio: 2.27.



Country: USA. Propellants: Lox/Kerosene. Agency: Rocketdyne. Bibliography: 225.

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