1.

Two satellites A and B go around a planet in circular orbits of radii 4 R and R respectively. If the speed of the satellite A is 3 V, then the speed of the satellite B will beA. 12 VB. 3 VC. 6 VD. `(3V)/(2)`

Answer» Correct Answer - C
`(V_(2))/(V_(1))=sqrt((GM)/(r_(2))xx(r_(1))/(GM))=sqrt((4)/(1))=2`
`therefore V_(2)=2V_(1)=6V`


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