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. is moving upwards at and discharges of fuel with a velocity of measured relative to the rocket. Assuming the exhaust nozzle has a crosssectional area of determine the volumetric flow rate of the exhaust gases at the nozzle and the rocket thrust. pts
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