In a rocket of mass 1000 kg fuel is consumed at a rate of 40 kg/s .The velocity of the gases ejected from the rocket is 5×10^4 m/s .The thrust on the rocke

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In a rocket of mass 1000 kg fuel is consumed at a rate of 40 kg/s. The velocity of the gases ejected from the rocket is $5 \times 10^{4}$ m/s. The thrust on the rocket is

Q. In a rocket of mass

1000 k g

fuel is consumed at a rate of

40 k g / s .

The velocity of the gases ejected from the rocket is

5000 m / s .

the thrust on the rocket is

Q. Fuel is consumed at the rate of

100 k g / s

in a rocket. The exhaust gases are ejected at a speed of

4.5 \times 10^{- 4} m / s

. Then the thrust experienced by the rocket is :

Q. A rocket of mass

1000 k g

is exhaust gases at a rate of

4 k g / s

with a velocity

3000 m / s

. The thrust developed on the rocket is

Q. A rocket has a mass of

1000 kg

with

50, 000 kg

of fuel being stored on this rocket. The nozzle of the rocket lets out the exhaust gases at a speed of

500 m/s

. If the rocket consumes fuel at the rate of

100 kg/s

, what is the acceleration of the rocket after

5 minutes

in a gravity free space?

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