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If the distance between the earth and th...

If the distance between the earth and the sun were half its present value, the number of days in a year would have been

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To solve the problem of how many days there would be in a year if the distance between the Earth and the Sun were half its present value, we can use Kepler's Third Law of Planetary Motion. Here’s a step-by-step breakdown of the solution: ### Step 1: Understand Kepler's Third Law Kepler's Third Law states that the square of the orbital period (T) of a planet is directly proportional to the cube of the semi-major axis (R) of its orbit. Mathematically, this is expressed as: \[ T^2 \propto R^3 \] This means: \[ \frac{T_1^2}{T_2^2} = \frac{R_1^3}{R_2^3} \] ### Step 2: Define the Variables Let: - \( T_1 \) = current orbital period of Earth = 365 days - \( R_1 \) = current distance between Earth and Sun = \( d \) - \( T_2 \) = new orbital period we want to find - \( R_2 \) = new distance between Earth and Sun = \( \frac{d}{2} \) ### Step 3: Apply Kepler's Law Using the relationship from Kepler's Third Law: \[ \frac{T_1^2}{T_2^2} = \frac{R_1^3}{R_2^3} \] Substituting the values: \[ \frac{365^2}{T_2^2} = \frac{d^3}{\left(\frac{d}{2}\right)^3} \] ### Step 4: Simplify the Right Side Calculating the right side: \[ \frac{d^3}{\left(\frac{d}{2}\right)^3} = \frac{d^3}{\frac{d^3}{8}} = 8 \] Thus, we have: \[ \frac{365^2}{T_2^2} = 8 \] ### Step 5: Solve for \( T_2^2 \) Rearranging gives: \[ T_2^2 = \frac{365^2}{8} \] ### Step 6: Calculate \( T_2 \) Taking the square root: \[ T_2 = \sqrt{\frac{365^2}{8}} = \frac{365}{\sqrt{8}} = \frac{365}{2\sqrt{2}} = \frac{365}{2 \times 1.414} \approx \frac{365}{2.828} \approx 129 \] ### Conclusion Thus, if the distance between the Earth and the Sun were half its present value, the number of days in a year would be approximately **129 days**. ---

To solve the problem of how many days there would be in a year if the distance between the Earth and the Sun were half its present value, we can use Kepler's Third Law of Planetary Motion. Here’s a step-by-step breakdown of the solution: ### Step 1: Understand Kepler's Third Law Kepler's Third Law states that the square of the orbital period (T) of a planet is directly proportional to the cube of the semi-major axis (R) of its orbit. Mathematically, this is expressed as: \[ T^2 \propto R^3 \] This means: ...
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