Advertisement Remove all ads

If the Height of a Satellite Completing One Revolution Around the Earth in T Seconds is H1 Meter, Then What Would Be the Height of a Satellite Taking 2 √ 2 T Seconds for One Revolution? - Science and Technology 1

Advertisement Remove all ads
Advertisement Remove all ads
Advertisement Remove all ads
Answer in Brief

Solve the problem.

If the height of a satellite completing one revolution around the earth in T seconds is h1 meter, then what would be the height of a satellite taking  \[2\sqrt{2} T\] seconds for one revolution?

Advertisement Remove all ads

Solution

 Time period of the satellite is given as

\[T = \frac{2\pi(R + h)\sqrt{R + h}}{\sqrt{GM}}\]
When the height of the satellite is h1, it takes T time to revolve around the Earth.
Thus, 
\[T = \frac{2\pi(R + h_1 )\sqrt{R + h_1}}{\sqrt{GM}} = \frac{2\pi(R + h_1 )^\frac{3}{2}}{\sqrt{GM}}\]  ....(i)
When the satellite takes \[2\sqrt{2} T\]  time to revolve around the Earth, let it be at height h2. Thus,
\[2\sqrt{2}T = \frac{2\pi(R + h_2 )\sqrt{R + h_2}}{\sqrt{GM}} = \frac{2\pi \left( R + h_2 \right)^\frac{3}{2}}{\sqrt{GM}}\]
Dividing (ii) by (i), we get
\[2\sqrt{2} = \frac{\left( R + h_2 \right)^\frac{3}{2}}{\left( R + h_1 \right)^\frac{3}{2}}\]
\[ \Rightarrow \frac{R + h_2}{R + h_1} = 2\]
\[ \Rightarrow h_2 = R + 2 h_1\]
Concept: Orbits of Artificial Satellites
  Is there an error in this question or solution?
Advertisement Remove all ads
Share
Notifications

View all notifications


      Forgot password?
View in app×