The exhaust velocity of the gases coming out of a rocket is 350 m/s w.r.t the rocket. The rocket can burn fuel at a rate of 80 kg/s. For a successful launch, the desired acceleration of the rocket is 4 m/s2. What is the initial total mass of this rocket? (Take g=10 m/s2)

The exhaust velocity of the gases coming out of a rocket is 350 m/s w.

1.	The exhaust velocity of the gases coming out of a rocket is 350 m/s w.r.t the rocket. The rocket can burn fuel at a rate of 80 kg/s. For a successful launch, the desired acceleration of the rocket is 4 m/s2. What is the initial total mass of this rocket? (Take g=10 m/s2)
Answer» The exhaust velocity of the gases coming out of a rocket is $350 m/s$ w.r.t the rocket. The rocket can burn fuel at a rate of $80 kg/s$ . For a successful launch, the desired acceleration of the rocket is $4 {m/s}^{2}$ . What is the initial total mass of this rocket? (Take $g = 10 {m/s}^{2}$ )

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The exhaust velocity of the gases coming out of a rocket is 350 m/s w.r.t the rocket. The rocket can burn fuel at a rate of 80 kg/s. For a successful launch, the desired acceleration of the rocket is 4 m/s2. What is the initial total mass of this rocket? (Take g=10 m/s2)

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