If Ve is the escape velocity of a body from a planet of mass M and radius R. Then the velocity of the satellite revolving at height h from the surface of the planet will be:
A
Ve√RR+h
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B
Ve√2RR+h
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C
Ve√R+hR
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D
Ve√R2(R+h)
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Solution
The correct option is DVe√R2(R+h) Escape velocity, ve=√2GMeR