Which of the following variables is not useful in the determination of rocket effective exhaust velocity?

A)
Rocket velocity
B)
Exit area
C)
Mass flow rate
D)
Exhaust velocity

Correct Answer :   Rocket velocity


Explanation : In the formulation of effective exhaust velocity, mass flow rate, exhaust velocity, exit area, nozzle exit pressure, ambient pressure are all relevant variables. But the rocket velocity doesn’t come into picture in the final expression.