A satellite revolving around in orbit of the Earth at a radius rand a velocity v. If the radius of its orbit becomes doubled, Find out its new velocity?
A
v/2
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B
v/√2
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C
v
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D
√2v
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E
2v
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Solution
The correct option is Bv/√2 Orbital velocity v of a satellite revolving in an orbit of radius r is given by
v=√GM/r
now if the radius is doubled , new velocity v′=√GM/2r=√GM/r×√1/2