The radii of circular orbits of two satellites A and B of the earth are 4R and R, respectively. if the speed of satellite A is 3v, then the speed of satellite B will be:
A
3v/4
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B
6v
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C
12v
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D
3v/2
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Solution
The correct option is B 6v =√GMRVAVB=√rBrA=√R4R=12∴VAVB=3VVB=12∴VB=6V