Answer is : (d) \(T\propto (r_1+r_2)^{\frac{3}{2}}\)
The semi-major axis of the elliptical orbit around the sun is given by
\(r=\frac{r_1+r_2}{2}\)
According to Kepler’s third law,
\(T^2\propto r^3\)
\(\Rightarrow T^2\propto (\frac{r_1+r_2}{2})^3\)
\(or\: T\propto (\frac{r_1+r_2}{2})^\frac{3}{2}\)
\(or\:T\propto (r_1+r_2)^{\frac{3}{2}}\)