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If W is the weight of a satellite on the surface of the earth, then the energy required to launch that satellite from the surface of earth into a circular orbit of radius 3R is (here R is the radius of earth)

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5WR/6

6WR/5

2WR/3

3WR/2

answer is A.

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Detailed Solution

w = Total energy in orbit - gravitational potential energy on surface of planet

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