Two satellites have their masses in the ratio 3:1. The radii of their circular orbits are in the ratio 1:4. What is the total mechanical energy of A and B?
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Total energy T.E.=
2r
−GMm
Now Total energy for p, T
p
=
2r
p
−GMm
similarly T
q
=
2r
q
−GMm
Taking the ratio we get,
T
q
T
p
=
2r
p
−GMm
×
−GMm
2r
q
=
r
p
r
q
. Given
r
q
r
p
=3.
Therefore,
T
q
T
p
=
3
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