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, E∝mr
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.