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Question: A small planet is revolving around a very massive star in a circular orbit of radius \(R\) with a pe...

A small planet is revolving around a very massive star in a circular orbit of radius RR with a period of revolution TT. If the gravitational force between the planet and the star were proportional to R52{R^{\dfrac{{ - 5}}{2}}}, then TT would be proportional to:
A) R32{R^{\dfrac{3}{2}}}
B) R35{R^{\dfrac{3}{5}}}
C) R72{R^{\dfrac{7}{2}}}
D) R74{R^{\dfrac{7}{4}}}

Explanation

Solution

In this problem, it is given that the planet is revolving around the star, this revolution is due to the gravitational force between the star and the planet. By equating the gravitational force between two masses formula and the motion of the object in circular path formula, the period of revolution is determined.

Useful formula:
Gravitational force between two masses,
F=Gm1m2r2F = \dfrac{{G{m_1}{m_2}}}{{{r^2}}}
Where, FF is the force, GG is the gravitational constant, m1{m_1} is the mass of the first object, m2{m_2} is the mass of the second object and rr is the distance between the two masses.

Motion of the object in circular orbit,
F=m×r×ω2F = m \times r \times {\omega ^2}
Where, FF is the force, mm is the mass of the revolving object, rr is the circular radius and ω\omega is the angular velocity.

Complete step by step solution:
Given that,
The gravitational force is proportional to the R52{R^{\dfrac{{ - 5}}{2}}}.
Then, the gravitational force is written as,
F=G×M×mR52..................(1)F = \dfrac{{G \times M \times m}}{{{R^{\dfrac{5}{2}}}}}\,..................\left( 1 \right)
Here, MM is the mass of the star and mm is the mass of the planet.
Now,
Motion of the object in circular orbit,
F=m×R×ω2..............(2)F = m \times R \times {\omega ^2}\,..............\left( 2 \right)
Here, mm is the mass of the planet.
Now equating the equation (1) and equation (2), then
G×M×mR52=m×R×ω2................(3)\dfrac{{G \times M \times m}}{{{R^{\dfrac{5}{2}}}}} = m \times R \times {\omega ^2}\,................\left( 3 \right)
By cancelling the mass of the planet mm on both sides, then the above equation is written as,
G×MR52=R×ω2\dfrac{{G \times M}}{{{R^{\dfrac{5}{2}}}}} = R \times {\omega ^2}
Now, the angular velocity is also written as ω=2πT\omega = \dfrac{{2\pi }}{T}, where TT is the period of revolution. And substitute this in the above equation,
G×MR52=R×(2πT)2\dfrac{{G \times M}}{{{R^{\dfrac{5}{2}}}}} = R \times {\left( {\dfrac{{2\pi }}{T}} \right)^2}
By squaring the term 2πT\dfrac{{2\pi }}{T} in RHS, then
G×MR52=R×4π2T2\dfrac{{G \times M}}{{{R^{\dfrac{5}{2}}}}} = R \times \dfrac{{4{\pi ^2}}}{{{T^2}}}
By taking the RR from RHS to LHS, then the above equation is written as,
G×MR52×R1=4π2T2\dfrac{{G \times M}}{{{R^{\dfrac{5}{2}}} \times {R^1}}} = \dfrac{{4{\pi ^2}}}{{{T^2}}}
By adding the power of RR in the LHS, then
G×MR52+1=4π2T2\dfrac{{G \times M}}{{{R^{\dfrac{5}{2} + 1}}}} = \dfrac{{4{\pi ^2}}}{{{T^2}}}
On further calculation, then
G×MR72=4π2T2\dfrac{{G \times M}}{{{R^{\dfrac{7}{2}}}}} = \dfrac{{4{\pi ^2}}}{{{T^2}}}
To find the period of revolution, so keep TT in one side and other terms in other side, then
T2=4π2×R72G×M{T^2} = \dfrac{{4{\pi ^2} \times {R^{\dfrac{7}{2}}}}}{{G \times M}}
Assume the term 4π2GM\dfrac{{4{\pi ^2}}}{{GM}} as constant, then
T2R72{T^2} \propto {R^{\dfrac{7}{2}}}
TR74{T} \propto {R^{\dfrac{7}{4}}}

Hence, the option (D) is correct.

Note: Here the distance between the star and the planet is equal to the radius of the revolution, so in the equation (2), the radius of the planet revolution rr is taken as RR, which is equal to the distance between the star and the planet which is taken in the gravitational force equation.