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In a rocket of mass 1000 kg fuel is cons...

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 `5xx10^(4)m//s`. The thrust on the rocket is

A

`2xx10^(6)N`

B

`2xx10^(4)N`

C

`2xx10^(3)N`

D

zero

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The correct Answer is:
A
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