Step 1: Understanding the Concept:
Kepler's Third Law relates the orbital period to the orbital radius and the mass of the central body.
Key Formula or Approach:
\( T^{2} = \frac{4\pi^{2}r^{3}}{GM} \).
Mass \( M = \rho \times \text{Volume} = \rho \times \frac{4}{3}\pi R^{3} \).
Step 2: Detailed Explanation:
1. Initial Case: Period \( T \) at radius \( r \) around star of mass \( M \).
2. Final Case:
$\bullet$ Orbital radius becomes \( r' = r/2 \).
$\bullet$ Star radius becomes \( R' = R/2 \). Since density \( \rho \) is constant, the new mass is \( M' = \rho \frac{4}{3}\pi (R/2)^{3} = M/8 \).
3. New Period \( T' \):
\[ (T')^{2} \propto \frac{(r/2)^{3}}{M/8} = \frac{r^{3}/8}{M/8} = \frac{r^{3}}{M} \]
Since the ratio \( r^{3}/M \) remains the same, \( (T')^{2} = T^{2} \).
Step 3: Final Answer:
The time period remains unchanged as T.