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The ratio of the distance of two planets...

The ratio of the distance of two planets from the sun is `1:2`. Then ratio of their priods of revolutions is

A

`1:4`

B

`1:sqrt2`

C

`1:2`

D

`1:2sqrt2`

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The correct Answer is:
To solve the problem, we will use Kepler's Third Law of planetary motion, which states that the square of the period of revolution (T) of a planet is directly proportional to the cube of the semi-major axis (R) of its orbit around the sun. Mathematically, this can be expressed as: \[ T^2 \propto R^3 \] Given that the ratio of the distances of two planets from the sun is \( R_1 : R_2 = 1 : 2 \), we can denote the distances as: \[ R_1 = 1 \text{ unit} \] \[ R_2 = 2 \text{ units} \] Now, we will find the ratio of their periods of revolution \( T_1 : T_2 \). ### Step 1: Write Kepler's Third Law for both planets From Kepler's Third Law, we have: \[ T_1^2 \propto R_1^3 \] \[ T_2^2 \propto R_2^3 \] ### Step 2: Express the proportionality in terms of a constant We can express these relationships as: \[ T_1^2 = k R_1^3 \] \[ T_2^2 = k R_2^3 \] where \( k \) is a constant of proportionality. ### Step 3: Substitute the values of \( R_1 \) and \( R_2 \) Substituting \( R_1 = 1 \) and \( R_2 = 2 \): \[ T_1^2 = k (1)^3 = k \] \[ T_2^2 = k (2)^3 = k \cdot 8 \] ### Step 4: Find the ratio \( T_1^2 : T_2^2 \) Now, we can find the ratio of the squares of the periods: \[ \frac{T_1^2}{T_2^2} = \frac{k}{8k} = \frac{1}{8} \] ### Step 5: Take the square root to find the ratio of the periods To find the ratio of the periods \( T_1 : T_2 \), we take the square root of both sides: \[ \frac{T_1}{T_2} = \sqrt{\frac{1}{8}} = \frac{1}{\sqrt{8}} = \frac{1}{2\sqrt{2}} \] ### Final Ratio Thus, the ratio of their periods of revolution is: \[ T_1 : T_2 = 1 : 2\sqrt{2} \]

To solve the problem, we will use Kepler's Third Law of planetary motion, which states that the square of the period of revolution (T) of a planet is directly proportional to the cube of the semi-major axis (R) of its orbit around the sun. Mathematically, this can be expressed as: \[ T^2 \propto R^3 \] Given that the ratio of the distances of two planets from the sun is \( R_1 : R_2 = 1 : 2 \), we can denote the distances as: \[ R_1 = 1 \text{ unit} \] \[ R_2 = 2 \text{ units} \] ...
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