Solveeit Logo

Question

Question: The radius of a planet is \(R_1\), and a satellite revolves around it in a radius \(R_2\) time perio...

The radius of a planet is R1R_1, and a satellite revolves around it in a radius R2R_2 time period of revolution is T. Find the acceleration due to gravity.

A. 4π2R23R12T2\dfrac{{4{\pi ^2}{\rm{R}}_2^3}}{{{\rm{R}}_1^2{{\rm{T}}^2}}}

B. 4π2R23R1T2\dfrac{{4{\pi ^2}{\rm{R}}_2^3}}{{{{\rm{R}}_1}{{\rm{T}}^2}}}

C. 2π2R23R1T2\dfrac{{2{\pi ^2}{\rm{R}}_2^3}}{{{{\rm{R}}_1}{{\rm{T}}^2}}}

D. 4π2R2T2\dfrac{{4{\pi ^2}{{\rm{R}}_2}}}{{{{\rm{T}}^2}}}

Explanation

Solution

We know that there are satellites revolving around the earth. It is because the satellite is revolving around earth due to the gravitational attraction between earth and the satellite. The centripetal force required to maintain the satellite in its orbit is provided by the gravitational attraction of the earth.

Complete step by step answer:

Let us assume that the orbit of the satellite is circular, and the satellite is revolving around the earth in a circular path. The gravitational force between the earth (mass M) and the satellite (mass m) provide a centripetal force to the satellite to move in a circular orbit.

i.e. centripetal force = gravitational force

mv2R=GMmR2\dfrac{{m{v^2}}}{{\rm{R}}} = \dfrac{{GMm}}{{{{\rm{R}}^2}}}

GMR=v2 \Rightarrow \dfrac{{GM}}{R} = {v^2}

Now, the velocity of the satellite is v = 2πRT\dfrac{{2\pi R}}{T}

Where 2πR is the circumference of the circle, and T is the time period.

Substitute the value of velocity in the above equation, we get

GMR=4π2RT22\dfrac{{GM}}{R} = {\dfrac{{4{\pi ^2}R}}{{{T^2}}}^2}

GM=4π2R3T2 \Rightarrow GM = \dfrac{{4{\pi ^2}{R^3}}}{{{T^2}}}

T2=4π2R3GM\therefore {T^2} = \dfrac{{4{\pi ^2}{R^3}}}{{GM}}

We use this relation to solve the above problem, let two radii R1R_1 (planet) and R2R_2 (satellite).

Now the time period of a satellite revolving around the planet of mass MM in radius R2R_2 is given as,

GM=4π2R23T2GM = \dfrac{{4{\pi ^2}{R_2}^3}}{{{T^2}}}

Also, acceleration due to gravity of the planet of mass MM of radius R1R_1 is given as,

g=GMR12g = \dfrac{{GM}}{{R_1^2}}

Put the value of GM in the second equation,

g=4π2R23R12T2g = \dfrac{{4{\pi ^2}{R_2}^3}}{{R_1^2{T^2}}}

Hence the correct option is (A).

Note:
The acceleration experienced by a body due to the gravitational force of the earth is known as acceleration due to gravity. Here “g” is the vector quantity; it depends on the mass of the planet and radius of the planet. It is independent of mass of the body. Also, the value of g is different for different heavy bodies.