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A satellite is launched into a circular ...

A satellite is launched into a circular orbit of radius 'R' around earth while a second satellite is launched into an orbit or radius 1.02 R. The percentage difference in the time periods of the two satellites is

A

0.7

B

`1.0`

C

`1.5`

D

3

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The correct Answer is:
To find the percentage difference in the time periods of two satellites in circular orbits around the Earth, we can follow these steps: ### Step 1: Understand the relationship between the time period and the radius of the orbit. The time period \( T \) of a satellite in a circular orbit is given by Kepler's third law, which states that: \[ T^2 \propto r^3 \] This means that the square of the time period is directly proportional to the cube of the radius of the orbit. ### Step 2: Set up the relationship for both satellites. Let the radius of the first satellite's orbit be \( R \) and its time period be \( T_1 \). For the second satellite, which is in an orbit of radius \( 1.02R \), let the time period be \( T_2 \). According to Kepler's third law: \[ T_1^2 \propto R^3 \] \[ T_2^2 \propto (1.02R)^3 \] ### Step 3: Express the time periods in terms of the radius. From the proportionality, we can write: \[ T_1^2 = kR^3 \quad \text{(1)} \] \[ T_2^2 = k(1.02R)^3 = k(1.02^3R^3) \quad \text{(2)} \] where \( k \) is a constant. ### Step 4: Calculate \( T_2 \) in terms of \( T_1 \). From equation (1) and (2): \[ T_2^2 = 1.02^3 kR^3 \] Taking the square root to find \( T_2 \): \[ T_2 = \sqrt{1.02^3} \cdot \sqrt{kR^3} = \sqrt{1.02^3} \cdot T_1 \] ### Step 5: Calculate \( \sqrt{1.02^3} \). Calculating \( 1.02^3 \): \[ 1.02^3 = 1.061208 \] Thus, \[ T_2 \approx 1.0305 T_1 \] ### Step 6: Find the percentage difference in the time periods. The percentage difference in time periods can be calculated as: \[ \text{Percentage difference} = \frac{T_2 - T_1}{T_1} \times 100\% \] Substituting \( T_2 \): \[ \text{Percentage difference} = \frac{(1.0305 T_1 - T_1)}{T_1} \times 100\% \] \[ = (1.0305 - 1) \times 100\% \] \[ = 0.0305 \times 100\% \approx 3.05\% \] ### Final Answer: The percentage difference in the time periods of the two satellites is approximately **3.05%**. ---

To find the percentage difference in the time periods of two satellites in circular orbits around the Earth, we can follow these steps: ### Step 1: Understand the relationship between the time period and the radius of the orbit. The time period \( T \) of a satellite in a circular orbit is given by Kepler's third law, which states that: \[ T^2 \propto r^3 \] This means that the square of the time period is directly proportional to the cube of the radius of the orbit. ...
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