A classical mechanics problem by Christian Leonardi

a rocket of a mass M is moving with an acceleration a vertically upward from the ground. The exhaust speed is v . the fuel consumption is 12,000kg/s find the upward acceleration. (in km s^-2)

info: g=9.8 v=1000 m/s M=1 Mega gram Air temp=300 K P=1 atm

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