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The time period of a satellite in a circ...

The time period of a satellite in a circular orbit around the earth is T . The kinetic energy of the satellite is proportional to `T^(-n)` . Then, n is equal to :

A

`(1)/(2)`

B

`(2)/(3)`

C

`(4)/(3)`

D

`(3)/(2)`

Text Solution

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The correct Answer is:
To solve the problem, we need to find the relationship between the kinetic energy of a satellite in a circular orbit and its time period \( T \). We will derive the relationship step by step. ### Step 1: Understand the Kinetic Energy Formula The kinetic energy \( KE \) of an object is given by the formula: \[ KE = \frac{1}{2} m v^2 \] where \( m \) is the mass of the satellite and \( v \) is its velocity. ### Step 2: Find the Velocity of the Satellite For a satellite in a circular orbit, the velocity \( v \) can be expressed in terms of the radius \( r \) of the orbit and the time period \( T \): \[ v = \frac{2\pi r}{T} \] This is because the satellite travels a distance of \( 2\pi r \) in one complete orbit, which takes time \( T \). ### Step 3: Substitute Velocity into the Kinetic Energy Formula Now, substituting the expression for \( v \) into the kinetic energy formula: \[ KE = \frac{1}{2} m \left(\frac{2\pi r}{T}\right)^2 \] This simplifies to: \[ KE = \frac{1}{2} m \cdot \frac{4\pi^2 r^2}{T^2} = \frac{2\pi^2 m r^2}{T^2} \] ### Step 4: Relate Radius \( r \) to Time Period \( T \) According to Kepler's Third Law, the time period \( T \) is related to the radius \( r \) of the orbit: \[ T^2 \propto r^3 \quad \Rightarrow \quad r \propto T^{2/3} \] This means we can express \( r \) in terms of \( T \): \[ r = k T^{2/3} \] where \( k \) is a proportionality constant. ### Step 5: Substitute \( r \) Back into the Kinetic Energy Expression Now, substituting \( r = k T^{2/3} \) into the kinetic energy equation: \[ KE = \frac{2\pi^2 m (k T^{2/3})^2}{T^2} \] This simplifies to: \[ KE = \frac{2\pi^2 m k^2 T^{4/3}}{T^2} = 2\pi^2 m k^2 T^{4/3 - 2} = 2\pi^2 m k^2 T^{-2/3} \] ### Step 6: Determine the Value of \( n \) From the expression \( KE \propto T^{-2/3} \), we can see that the kinetic energy is proportional to \( T^{-n} \) where \( n = \frac{2}{3} \). ### Final Answer Thus, the value of \( n \) is: \[ \boxed{\frac{2}{3}} \]

To solve the problem, we need to find the relationship between the kinetic energy of a satellite in a circular orbit and its time period \( T \). We will derive the relationship step by step. ### Step 1: Understand the Kinetic Energy Formula The kinetic energy \( KE \) of an object is given by the formula: \[ KE = \frac{1}{2} m v^2 \] where \( m \) is the mass of the satellite and \( v \) is its velocity. ...
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