Question:

satellite revolve in radius R has a time period of revolution T. Find time period of a satellite if orbital radius is 9R?

Updated On: Jul 28, 2022
  • $3\sqrt{3}T$
  • 9T
  • 27 T
  • $9\sqrt{3}T$
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The Correct Option is C

Solution and Explanation

According to Kepler's law of periods $T^{2}\,\propto\,R^{3}$ So,$\,\Rightarrow\, \frac{T_{1}}{T_{2}}=\left(\frac{R_{1}}{R_{2}}\right)^{\frac{3}{2}}$ $\Rightarrow\, \frac{T}{T_{2}}=\left(\frac{R}{9R}\right)^{\frac{3}{2}}\,=\frac{1}{27}\,\left[\because \,T_{1}=T\right]$ $T_{2}=27T$
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Concepts Used:

Keplers Laws

Kepler’s laws of planetary motion are three laws describing the motion of planets around the sun.

Kepler First law – The Law of Orbits

All the planets revolve around the sun in elliptical orbits having the sun at one of the foci.

Kepler’s Second Law – The Law of Equal Areas

It states that the radius vector drawn from the sun to the planet sweeps out equal areas in equal intervals of time.

Kepler’s Third Law – The Law of Periods

It states that the square of the time period of revolution of a planet is directly proportional to the cube of its semi-major axis.

T2 ∝ a3