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 assume a constant mass, in reality
the rocket would lose mass from fuel expenditure experiences of thrust
over a minute window and reaches an altitude of 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 minute mark?
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