Fuel aboard a rocket has a density of 2870 kgm3 and is


Fuel aboard a rocket has a density of 2870 kg/m^3 and is ejected with a speed of 2650 m/s. if the engine is to provide a thrust of 1.21 x 10^6 N, what volume of fuel must be burned per second? Answer in units of m^3/s.

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Physics: Fuel aboard a rocket has a density of 2870 kgm3 and is
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