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If v0 be the orbital velocity of a sate...

If `v_0` be the orbital velocity of a satellite in a circular orbit close to the earth's surface and `v_e` is the escape velocity from the earth, then relation between the two is .........

A

`v_o = sqrt(2v_c)`

B

`v_o =v_c`

C

`v_c = v_osqrt(2)`

D

`v_c=sqrt(2v_0)`

Text Solution

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The correct Answer is:
D
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