Question: ( b ) The rocket in Fig. 5 is moving upwards at 3 5 0 m s and discharges 6 0 k g s of

(b) The rocket in Fig. 5 is moving upwards at 350ms and discharges 60kgs of fuel with a velocity (Ve) of 3200ms measured relative to the rocket. Assuming the exhaust nozzle has a cross-sectional area of 0.06m2, determine the volumetric flow rate of the exhaust gases at the nozzle and the rocket thrust. [10pts.]
=6dkgkg's
( b ) The rocket in Fig. 5 is moving upwards at 3

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