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Larch HTP/Kerosene Rocket Engine

Larch HTP/Kerosene Rocket Engine

Bristol Siddeley Gamma 2 engine fueled with RP-1 (kerosine) and Peroxide as oxidizer.  The Gamma 2 or Double Gamma was a two chamber version, used for the second stage of the Black Arrow satellite launch vehicle. As the only Gamma not required to operate at sea level, the nozzles were extended to allow for better expansion of exhaust gases at high altitudes.

Bristol Siddeley Gamma 2 engine fueled with RP-1 (kerosine) and Peroxide as oxidizer. The Gamma 2 or Double Gamma was a two chamber version, used for the second stage of the Black Arrow satellite launch vehicle. As the only Gamma not required to operate at sea level, the nozzles were extended to allow for better expansion of exhaust gases at high altitudes.

RL10 rocket engine turbopump by Pratt & Whitney Rocketdyne. Used in American space program. [1856x2791] [OC]

RL10 rocket engine turbopump by Pratt & Whitney Rocketdyne. Used in American space program. [1856x2791] [OC]

Bristol Siddeley Gamma 2 HTP/Kerosene rocket engine

Bristol Siddeley Gamma 2 HTP/Kerosene rocket engine

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