It is defined as the ratio of thrust force produced to fuel


Specific Impulse is a performance specification of rocket engines. It is defined as the ratio of thrust force produced to fuel (and oxidizer)  consumption rate by weight (not by mass), weight being measured at the Earth's surface. Calculate the specific impulse for a rocket engine with nozzle speed (exhaust speed relative to the engine nozzle) U.

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Physics: It is defined as the ratio of thrust force produced to fuel
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