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The escape velocity for the earth is V(...

The escape velocity for the earth is `V_(e)` . The escape velocity for a planet whose radius `(1)/(4)` th radius of earth and mass haif that of earth is

A

`(v_(a))/(sqrt(2))`

B

`sqrt(2) v_(a)`

C

`2 v_(a)`

D

`(v_(a))/(2)`

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The correct Answer is:
To find the escape velocity for a planet whose radius is one-fourth that of Earth and mass is half that of Earth, we can follow these steps: ### Step 1: Understand the formula for escape velocity The escape velocity \( V \) from the surface of a celestial body is given by the formula: \[ V = \sqrt{\frac{2GM}{R}} \] where: - \( G \) is the universal gravitational constant, - \( M \) is the mass of the celestial body, - \( R \) is the radius of the celestial body. ### Step 2: Define the parameters for Earth Let: - Mass of Earth \( M_E = M \) - Radius of Earth \( R_E = R \) - Escape velocity from Earth \( V_E = \sqrt{\frac{2GM_E}{R_E}} \) ### Step 3: Define the parameters for the new planet For the new planet: - Mass \( M_P = \frac{1}{2} M_E = \frac{M}{2} \) - Radius \( R_P = \frac{1}{4} R_E = \frac{R}{4} \) ### Step 4: Write the escape velocity formula for the new planet Using the escape velocity formula for the new planet: \[ V_P = \sqrt{\frac{2GM_P}{R_P}} \] Substituting the values of \( M_P \) and \( R_P \): \[ V_P = \sqrt{\frac{2G \left(\frac{M}{2}\right)}{\frac{R}{4}}} \] ### Step 5: Simplify the expression Now simplify the expression: \[ V_P = \sqrt{\frac{2G \cdot \frac{M}{2}}{\frac{R}{4}}} = \sqrt{\frac{GM}{R} \cdot 4} = \sqrt{4 \cdot \frac{GM}{R}} = 2\sqrt{\frac{GM}{R}} \] ### Step 6: Relate it to the escape velocity of Earth We know that: \[ V_E = \sqrt{\frac{2GM}{R}} \] Thus, we can express \( V_P \) in terms of \( V_E \): \[ V_P = 2 \cdot \sqrt{\frac{GM}{R}} = 2 \cdot \frac{V_E}{\sqrt{2}} = \sqrt{2} \cdot V_E \] ### Final Answer The escape velocity for the planet is: \[ V_P = \sqrt{2} V_E \]

To find the escape velocity for a planet whose radius is one-fourth that of Earth and mass is half that of Earth, we can follow these steps: ### Step 1: Understand the formula for escape velocity The escape velocity \( V \) from the surface of a celestial body is given by the formula: \[ V = \sqrt{\frac{2GM}{R}} \] where: ...
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