Question:

Two satellites of mass $m$ and $9\,m$ are orbiting a planet in orbits of radius $R$. Their periods of revolution will be in the ratio of

Updated On: Mar 26, 2024
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The Correct Option is C

Approach Solution - 1

The Correct Option is (C): 1:1

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Approach Solution -2

Kepler’s third law states that the square of the period of revolution is proportional to the cube of the semi-major axis of the orbit.

From Kepler’s third law  T2=R3,

where, T = period of revolution for an object around a planet and

R = Radius of the orbit which is the same as the semi-major axis for a circular orbit.

Let the time period for satellite of mass m  = T1, and for satellite of mass 9m = T2, Let the radius of a satellite of mass m orbiting the planet = R1 and satellite of mass 9m orbiting the same planet be R2

So, for two satellites orbiting the same planet, the ratio of their periods of revolution  (T1 and T2) will be:

\(=>\frac{T^2_1}{T_2^2}=\frac{R^2_1}{T_2^3}\)

Given that both planet are orbiting the same planet, therefore R1=R2=R  and substituting the value in the above equation we get:

\(=>\frac{T^2_1}{T_2^2}=\frac{R^3}{R^3}=1\)

\(=>\frac{T_1}{T_2}=1\)

So, the ratio of their periods of revolution is 1. This means that the periods of revolution for the two satellites are the same, regardless of their masses. 

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Concepts Used:

Gravitation

In mechanics, the universal force of attraction acting between all matter is known as Gravity, also called gravitation, . It is the weakest known force in nature.

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,

  • F ∝ (M1M2) . . . . (1)
  • (F ∝ 1/r2) . . . . (2)

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

F ∝ M1M2/r2

F = G × [M1M2]/r2 . . . . (7)

Or, f(r) = GM1M2/r2

The dimension formula of G is [M-1L3T-2].