Step 1: Understanding the Concept:
This problem is an application of Kepler's Third Law of planetary motion. The law states that the square of the orbital period (T) of a planet is directly proportional to the cube of the semi-major axis of its orbit, which for a nearly circular orbit can be taken as the mean distance (R) from the sun.
Step 2: Key Formula or Approach:
Kepler's Third Law can be written as:
\[ T^2 \propto R^3 \quad \text{or} \quad \frac{T^2}{R^3} = \text{constant} \]
For two planets, A and B, we can write the relationship as:
\[ \left(\frac{T_A}{T_B}\right)^2 = \left(\frac{R_A}{R_B}\right)^3 \]
Step 3: Detailed Explanation:
We are given the following information:
The period of planet A is 27 times the period of planet B: \(T_A = 27 T_B \implies \frac{T_A}{T_B} = 27\).
The distance of A is X times the distance of B: \(R_A = X R_B \implies \frac{R_A}{R_B} = X\).
Substitute these into Kepler's law equation:
\[ (27)^2 = (X)^3 \]
We can write 27 as \(3^3\):
\[ (3^3)^2 = X^3 \]
\[ 3^6 = X^3 \]
To solve for X, we can take the cube root of both sides:
\[ X = (3^6)^{1/3} = 3^{6/3} = 3^2 = 9 \]
Step 4: Final Answer:
The value of X is 9.