The upward velocity of a rocket can be computed by the following formula:
where υ = upward velocity, u = velocity at which fuel is expelled relative to the rocket, m0 = initial mass of the rocket at time t = 0, q = fuel consumption rate, and g = downward acceleration of gravity (assumed constant = 9.81 m/s2). If u = 1850 m/s, m0 = 160,000 kg, and q = 2500 kg/s, determine how high the rocket will fly in 30 s.
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