First slide
Second law
Question

During the rocket propulsion, gases ejecting with velocity 1 km/s relative to rocket. The rate of fuel consumption is m10kg/s,where m is the instantaneous mass of the rocket. If air resistance varies according to equation f - 0.15 mv, then terminal velocity of the rocket is :

Moderate
Solution

At terminal velocity Fnet = 0
vgasdmdt=mg+f1000m10=10m+0.15mvv=600m/s

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