Final speed of the last portion of the ejected fuel


A rocket is to be launched from deep space where there is no gravitational field. 81% of the initial mass of the rocket is fuel and this fuel is ejected with a relative velocity of 2300 m/s. Assuming that all of the fuel is used, find the final speed of the last portion of the ejected fuel relative to a stationary observer. Please provide step-by-step method.

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Physics: Final speed of the last portion of the ejected fuel
Reference No:- TGS0151321

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