Question: A rocket initially at rest weighing 2 5 , 0 0 0 l b f ( assume a constant mass, in reality the rocket would

A rocket initially at rest weighing 25,000lbf(assume a constant mass, in reality
the rocket would lose mass from fuel expenditure) experiences 75,000lbf of thrust
over a 1 minute window and reaches an altitude of 115,000ft. Assuming
incompressible flow with a pitot tube placed on the nose cone of the rocket, what is
the total pressure at the nose cone at the 1 minute mark?
A rocket initially at rest weighing 2 5 , 0 0 0 l

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