The workdone to increase the radius of orbit of satellite of mass m reoling around a planet of mass m from orbit of radius r in to another orbit of radius 3r
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The gravitational force 'F' on satellite of mass 'm' revolving around the planet in the orbit of radius 'R' is
F=−
R
2
GMm
Where
G is gravitational constant
M is Mass of the planet.
The work done in increasing the radius of orbit of the satellite through 'dr' is
W=Fdr
but work done is equal to change in gravitational potential '−dV'
therefore
−dV=Fdr
V=−∫
R
3R
Fdr
V=−
R
2
GMm
∫
R
3R
−(Fdr)
V=GMm∫
R
3R
R
2
1
dr
V=
R
GMm
−
3R
GMm
V=
3R
2GMm
Thus work done to increase the radius of orbit of satellite is
3R
2GMm
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