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If a time period of revolution of a satellite around a planet in a circular orbit of radius r is T,then the period of revolution around planet in a circular orbit of radius 3r will beA. TB. 3TC. 9TD. `3sqrt3T`

Answer» Correct Answer - d
`T_(1)=KR^(3//2) and T_(2)=(3R)^(3//2)(T_(2))/(T_(1))=3sqrt3`


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