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Question

Two satellites A and B, have ratio of masses 3:1 are in circular orbits of radii r and 4r. Then ratio of total mechanical energy of A and B is

A
1:3
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B
3:1
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C
3:4
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D
12:1
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Solution

The correct option is D 12:1
The total mechanical energy of a satellite of mass m in a circular orbit of radius r around a planet of mass M is given by
E=GMm2r So, Emr

Given,
Ratio of the masses of the satellites, mAmB=31

Ratio of the orbits of the satellites,
rArB=r4r=14

Now, the ratio of the total meachanical energy,

EAEB=mAmB×rBrA

EAEB=31×41

EAEB=12:1

Hence, option (d) is the correct answer.

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