Q. Prove that the velocity of a rocket of mass ;mo' at the instant when its mass is m is given by v='vo'+ u ln mo/m where vo is the initial velocity of the rocket and u is the velocity of the exhaust gases relative to the rocket Ans correctly...And pls no spamming.I will even follow the ryt ans
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they out Rockets journey Momwntum is conserved .
so if MV = MoVo
Dv/Dm can be equated to Ratio of Mo/V
and Log come because residual mass is reacted to gain in velocity by burn
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