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A setellite os revolving very close to ...

A setellite os revolving very close to a planet of density p. The period of revolution of satellite is

A

`sqrt((3pi)/(DG))`

B

`((3pi)/(DG))^(3//2)`

C

`sqrt((3pi)/(2DG))`

D

`sqrt((3piG)/(D))`

Text Solution

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The correct Answer is:
A
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