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The escape velocity of a body from the s...

The escape velocity of a body from the surface of the earth is `V_(1)` and from an altitude equal to twice the radius of the earth, is, `V_(2)`. Then

A

`V_(1)=V_(2)`

B

`V_(1)=7V_(2)`

C

`V_(1)=sqrt(3)V_(2)`

D

`V_(1)=sqrt(2)V_(2)`

Text Solution

AI Generated Solution

The correct Answer is:
To find the relationship between the escape velocities \( V_1 \) (from the surface of the Earth) and \( V_2 \) (from an altitude equal to twice the radius of the Earth), we can follow these steps: ### Step 1: Write the formula for escape velocity The escape velocity \( V \) from a distance \( r \) from the center of the Earth is given by the formula: \[ V = \sqrt{\frac{2GM}{r}} \] where \( G \) is the gravitational constant and \( M \) is the mass of the Earth. ### Step 2: Calculate \( V_1 \) At the surface of the Earth, the distance \( r \) is equal to the radius of the Earth \( R \). Therefore, the escape velocity \( V_1 \) is: \[ V_1 = \sqrt{\frac{2GM}{R}} \] ### Step 3: Calculate \( V_2 \) When the body is at an altitude equal to twice the radius of the Earth, the total distance from the center of the Earth becomes: \[ r = R + 2R = 3R \] Now, we can calculate the escape velocity \( V_2 \) at this distance: \[ V_2 = \sqrt{\frac{2GM}{3R}} \] ### Step 4: Relate \( V_2 \) to \( V_1 \) Now, we can express \( V_2 \) in terms of \( V_1 \): \[ V_2 = \sqrt{\frac{2GM}{3R}} = \frac{1}{\sqrt{3}} \sqrt{\frac{2GM}{R}} = \frac{1}{\sqrt{3}} V_1 \] ### Step 5: Conclusion Thus, we find the relationship between \( V_1 \) and \( V_2 \): \[ V_2 = \frac{1}{\sqrt{3}} V_1 \quad \text{or} \quad V_1 = \sqrt{3} V_2 \] ### Final Answer The relationship between the escape velocities is: \[ V_1 = \sqrt{3} V_2 \] ---

To find the relationship between the escape velocities \( V_1 \) (from the surface of the Earth) and \( V_2 \) (from an altitude equal to twice the radius of the Earth), we can follow these steps: ### Step 1: Write the formula for escape velocity The escape velocity \( V \) from a distance \( r \) from the center of the Earth is given by the formula: \[ V = \sqrt{\frac{2GM}{r}} \] where \( G \) is the gravitational constant and \( M \) is the mass of the Earth. ...
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