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Question

The time period of a satellite in a circular orbit of radius R is T, the period of another satellite in a circular orbit of radius 4R is

A
4T
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B
T/4
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C
8T
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D
T/8
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Solution

The correct option is C 8T
T=2πR[(R+h)3g]1/2
Here (R+h) changes from R to 4R. Hence period of revolution changes from T to (43)1/2T=8T.

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