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Escape velocity on the surface of earth ...

Escape velocity on the surface of earth is 11.2 km/s . Escape velocity from a planet whose mass is the same as that of earth and radius 1/4 that of earth is

A

11.2 km/s

B

22.4 km/s

C

5.6 km/s

D

44.8 km/s

Text Solution

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To solve the problem of finding the escape velocity from a planet whose mass is the same as that of Earth but with a radius of 1/4 that of Earth, we can use the formula for escape velocity: \[ v_e = \sqrt{\frac{2GM}{R}} \] Where: - \( v_e \) is the escape velocity, - \( G \) is the universal gravitational constant (\( 6.674 \times 10^{-11} \, \text{m}^3/\text{kg s}^2 \)), - \( M \) is the mass of the planet, - \( R \) is the radius of the planet. ### Step 1: Identify the known values - The escape velocity on the surface of Earth \( v_{e, \text{Earth}} = 11.2 \, \text{km/s} = 11200 \, \text{m/s} \). - The mass of the planet \( M \) is the same as that of Earth. - The radius of the planet \( R = \frac{1}{4} R_{\text{Earth}} \). ### Step 2: Write the escape velocity for Earth For Earth, we can express the escape velocity as: \[ v_{e, \text{Earth}} = \sqrt{\frac{2GM_{\text{Earth}}}{R_{\text{Earth}}}} \] ### Step 3: Write the escape velocity for the new planet For the planet with radius \( \frac{1}{4} R_{\text{Earth}} \): \[ v_{e, \text{planet}} = \sqrt{\frac{2GM_{\text{Earth}}}{\frac{1}{4} R_{\text{Earth}}}} = \sqrt{\frac{2GM_{\text{Earth}} \cdot 4}{R_{\text{Earth}}}} = \sqrt{4} \cdot \sqrt{\frac{2GM_{\text{Earth}}}{R_{\text{Earth}}}} = 2 \cdot v_{e, \text{Earth}} \] ### Step 4: Calculate the escape velocity for the new planet Substituting the escape velocity of Earth: \[ v_{e, \text{planet}} = 2 \cdot 11.2 \, \text{km/s} = 22.4 \, \text{km/s} \] ### Final Answer The escape velocity from the planet whose mass is the same as that of Earth and radius is \( \frac{1}{4} \) that of Earth is \( 22.4 \, \text{km/s} \). ---

To solve the problem of finding the escape velocity from a planet whose mass is the same as that of Earth but with a radius of 1/4 that of Earth, we can use the formula for escape velocity: \[ v_e = \sqrt{\frac{2GM}{R}} \] Where: - \( v_e \) is the escape velocity, ...
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