Question:

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. $T^{2}=K r^{3}$ 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 $F=\frac{G M m}{r^{2}}$ here $G$ is gravitational constant. The relation between $G$ and $K$ is described as

Updated On: Jun 3, 2023
  • $GMK = 4\pi^2$
  • $K = G$
  • $K = \frac {1}{G}$
  • $GK = 4 \pi^2$
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The Correct Option is A

Solution and Explanation

As we know, orbital speed, $V_{\text {orb }}=\sqrt{\frac{G M}{r}}$ Time period $T =\frac{2 \pi r}{V_{\text {orb }}}=\frac{2 \pi r}{\sqrt{G M}} \sqrt{r}$ Squaring both sides, $T^{2}=\left(\frac{2 \pi r \sqrt{r}}{\sqrt{G M}}\right)^{2}=\frac{4 \pi^{2}}{G M} \cdot r^{3} $ $ \Rightarrow \frac{T^{2}}{r^{3}}=\frac{4 \pi^{2}}{G M}=K$ $ \Rightarrow G M K=4 \pi^{2}$.
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Concepts Used:

Newtons Law of Gravitation

Gravitational Force

Gravitational force is a central force that depends only on the position of the test mass from the source mass and always acts along the line joining the centers of the two masses.

Newton’s Law of Gravitation:

According to Newton’s law of gravitation, “Every particle in the universe attracts every other particle with a force whose magnitude is,

  • Directly proportional to the product of their masses i.e. F ∝ (M1M2) . . . . (1)
  • Inversely proportional to the square of the distance between their center i.e. (F ∝ 1/r2) . . . . (2)

By combining equations (1) and (2) we get,

F ∝ M1M2/r2

F = G × [M1M2]/r2 . . . . (7)

Or, f(r) = GM1M2/r2 [f(r)is a variable, Non-contact, and conservative force]