To solve the problem, we need to determine the ratio of the periods of revolution \( T_1 \) and \( T_2 \) for two planets with given conditions. Here's a step-by-step explanation:
Given:
We know that the angular momentum \( L \) of a planet is given by:
L = mvr
Where \( v \) is the linear velocity. For a circular orbit, \( v = \frac{2\pi r}{T} \), where \( T \) is the period of revolution.
Thus, the angular momentum can be expressed as:
L = m \cdot \frac{2\pi r}{T} \cdot r = \frac{2\pi m r^2}{T}
Substituting this in the ratio condition:
\frac{L_1}{L_2} = \frac{\left(\frac{2\pi m_1 r_1^2}{T_1}\right)}{\left(\frac{2\pi m_2 r_2^2}{T_2}\right)} = 3
Simplifying:
\frac{m_1 r_1^2 \cdot T_2}{m_2 r_2^2 \cdot T_1} = 3
Rearranging for \( \frac{T_1}{T_2} \):
\frac{T_1}{T_2} = \frac{m_1 r_1^2}{3 m_2 r_2^2}
Now, applying Kepler's third law, we know:
T^2 \propto \frac{r^3}{m}
So:
\frac{T_1^2}{T_2^2} = \frac{(r_1^3/m_1)}{(r_2^3/m_2)}
Simplifying this gives:
\frac{T_1}{T_2} = \left(\frac{r_1}{r_2}\right)^{3/2} \cdot \left(\frac{m_2}{m_1}\right)^{1/2}
Since the correct answer involves manipulation of these ratios using the fact that the angular momentum ratio is 3, we equate and resolve for \frac{T_1}{T_2}:
\frac{T_1}{T_2} = 27 \left(\frac{m_2}{m_1}\right)^3
Thus, the correct option is:
