A socker moves in the absence of externas
forces, accleration depends upon the tas
a=KE, where k is tue constant, Derive
ane enpression for the mass m' of the
rocket at ang instant if les intial mass
be mo and the exhaust gases escape with
a constant velocice u reative Jai (OH)
to the rocket id ma moe-k E where is
Nu
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the answer to the question is n u k e k
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