Step 1: Escape Velocity Formula
The escape velocity \( v_e \) from a celestial body is calculated using the formula: \[ v_e = \sqrt{\frac{2GM}{R}} \] where: - \( G \) represents the gravitational constant
- \( M \) is the mass of the body
- \( R \) is the radius of the body
Step 2: Original Planet's Escape Velocity
Consider an initial planet with mass \( M \) and radius \( R \). Its escape velocity is given by: \[ v_e = \sqrt{\frac{2GM}{R}} \]
Step 2: New Planet's Parameters
A new planet is introduced with the following parameters: - Mass: \( M’ = 2M \)
- Radius: \( R’ = 2R \)
Step 3: Calculate New Escape Velocity
Substitute the new parameters into the escape velocity formula: \[ v_e’ = \sqrt{\frac{2G \cdot 2M}{2R}} \] \[ = \sqrt{\frac{4GM}{2R}} \] \[ = \sqrt{2 \cdot \frac{2GM}{R}} \] \[ = \sqrt{2} \cdot \sqrt{\frac{2GM}{R}} \] The new escape velocity is \( v_e’ = \sqrt{2} v_e \), indicating it is increased by a factor of \( \sqrt{2} \).
Step 4: Alternative Approach
Observe that escape velocity is proportional to the square root of the ratio \( \frac{M}{R} \): \[ v_e \propto \sqrt{\frac{M}{R}} \] For the new planet: \[ \frac{M’}{R’} = \frac{2M}{2R} = \frac{M}{R} \] Since the ratio \( \frac{M}{R} \) remains constant, the escape velocity is also unchanged. Thus, the correct answer is option (1) \( v_e \).
Net gravitational force at the center of a square is found to be \( F_1 \) when four particles having masses \( M, 2M, 3M \) and \( 4M \) are placed at the four corners of the square as shown in figure, and it is \( F_2 \) when the positions of \( 3M \) and \( 4M \) are interchanged. The ratio \( \dfrac{F_1}{F_2} = \dfrac{\alpha}{\sqrt{5}} \). The value of \( \alpha \) is 
