The rocket shown in Fig. P5.61 is held stationary by the horizontalforce, Fx, and the

Chapter 5, Problem 5.61

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The rocket shown in Fig. P5.61 is held stationary by the horizontalforce, Fx, and the vertical force, Fz. The velocity and pressureof the exhaust gas are 5000 ft/s and 20 psia at the nozzle exit, whichhas a cross section area of 60 in.2. The exhaust mass flowrate isconstant at 21 lbm/s. Determine the value of the restraining force Fx.Assume the exhaust flow is essentially horizontal.

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