Two satellites A and B go round the planet P in circular orbits having radii 4R and R respectively. If the speed of the satellite A is 3v, then the speed of satellite B will be
6v
3v2
12v
4v3
A
12v
B
4v3
C
6v
D
3v2
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Solution
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Velocity v of a satellite varies inversely as the square root of the orbit of radius r v∝1√r ∴VAVB=√rBrA=√R4R ⇒3vVB=12⇒VB=6v
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