Step 1: {Kepler’s third law}
\[
T^2 \propto R^3
\]
Step 2: {Find new time period}
\[
\left( \frac{T_2}{T_1} \right)^2 = \left( \frac{R_2}{R_1} \right)^3
\]
Substituting values:
\[
T_2 = \left( \frac{3R}{R} \right)^{3/2} \times 1
\]
\[
= 3\sqrt{3} { years}
\]
Thus, the correct answer is \( 3\sqrt{3} \) years.
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Approach Solution -2
Step 1: According to Kepler’s Third Law:
\( T^2 \propto R^3 \), where:
- \( T \) is the time period (orbital duration)
- \( R \) is the radius (mean distance from the Sun)
Step 2: Let the current time period be \( T_1 = 1 \) year for distance \( R \).
Let the new time period be \( T_2 \) when the distance becomes \( 3R \).
Step 3: Use the ratio form of Kepler’s law:
\( \left( \frac{T_2}{T_1} \right)^2 = \left( \frac{R_2}{R_1} \right)^3 \)
\( \left( \frac{T_2}{1} \right)^2 = (3)^3 = 27 \)
\( T_2 = \sqrt{27} = 3\sqrt{3} \) years