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A rocket burns large amounts of fuel, hence it's mass decreases significantly in flight. The velocity of a rocket t minuted after liftoff can be estimated by the formula v(t) = -gt-kln((M-ct)/M) where g is gravitational acceleration, k is the speed at which exhaust gas is ejected, c is the rate of fuel consumption, and M is the initial mass of the rocket (fuel included). Find the height h(t) of the rocket, as a function of time. HELP!
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integrate the given function !
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