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Question: Kepler's third law states that square of period of revolution (T) of a planet around the sun, is pro...

Kepler's third law states that square of period of revolution (T) of a planet around the sun, is proportional to third power of average distance r between sun and planet i.e. T2=Kr3{T^2} = K{r^3} , here K is constant. If the masses of sun and planet are M and m respectively then as per Newton's law of gravitation force of attraction between them is F=GMm2F = \dfrac{{GMm}}{2} , here G is gravitational constant. The relation between G and K is described as
A. GMK=4π2GMK = 4{\pi ^2}
B. K=G
C. K=1GK = \dfrac{1}{G}
D. GK=4π2GK = 4{\pi ^2}

Explanation

Solution

The planets’ orbital circular motion is controlled by the centripetal force exerted by gravitation. Therefore, GMmr2=mv2r\dfrac{{GMm}}{{{r^2}}} = \dfrac{{m{v^2}}}{r}. So, the time period of the planets for one complete revolution is T=2πrv=2πrGMrT = \dfrac{{2\pi r}}{v} = \dfrac{{2\pi r}}{{\sqrt {\dfrac{{GM}}{r}} }}. Now T2=Kr3{T^2} = K{r^3}, given. Equate all these relations and simplify to get the relation between K and G.
Complete step-by-step solution:
The planets’ orbital circular motion is controlled by the centripetal force exerted by gravitation.
Therefore, GMmr2=mv2r\dfrac{{GMm}}{{{r^2}}} = \dfrac{{m{v^2}}}{r}
GMr=v2\Rightarrow \dfrac{{GM}}{r} = {v^2}
v=GMr\Rightarrow v = \sqrt {\dfrac{{GM}}{r}}
So, the time period of the planets for one complete revolution is T=2πrv=2πrGMrT = \dfrac{{2\pi r}}{v} = \dfrac{{2\pi r}}{{\sqrt {\dfrac{{GM}}{r}} }}
Squaring each side, we have
T2=4π2r2GMr{T^2} = \dfrac{{4{\pi ^2}{r^2}}}{{\dfrac{{GM}}{r}}}
T2=4π2r3GM\Rightarrow {T^2} = \dfrac{{4{\pi ^2}{r^3}}}{{GM}}
KGM=4π2\Rightarrow KGM = 4{\pi ^2}

Therefore, the correct answer is option (A).

Note:
Note that orbital circular motion of the planets is controlled by the centripetal force exerted by gravitation. Again, the time period of the planets for one complete revolution is T=2πrv=2πrGMrT = \dfrac{{2\pi r}}{v} = \dfrac{{2\pi r}}{{\sqrt {\dfrac{{GM}}{r}} }}.