Physics, asked by Kapue9412, 9 months ago

For a rocket propulsion velocity of exhaust gases

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Answered by pawarshubhangi076
1

Answer:

For a rocket propulsion velocity of exhaust gasas relative to rocket 2 km/s.

If mass of system rocket is 1000 kg then the rate of fual is consumption of a rocket to rise up with an acceleration 4.

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