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A body mass 'm' is dropped from heinght ...

A body mass 'm' is dropped from heinght `R/2`, from earth's surface, where 'R' is the radius of earth. Its speed when it will hit the earth's surface is `(v_(e)="escape velocity from earth's surface")`.

A

`sqrt3 v_(e)`

B

`(v_(e))/(sqrt3)`

C

`(v_(e))/(sqrt2)`

D

`sqrt2 v_(e)`

Text Solution

AI Generated Solution

The correct Answer is:
To solve the problem of finding the speed of a body dropped from a height of \( R/2 \) above the Earth's surface when it hits the Earth's surface, we can use the principle of conservation of energy. Here's a step-by-step solution: ### Step 1: Understand the Initial and Final Potential Energy 1. **Initial Height**: The body is dropped from a height of \( R/2 \) above the Earth's surface. Therefore, the distance from the center of the Earth is: \[ R + \frac{R}{2} = \frac{3R}{2} \] 2. **Final Height**: When the body hits the Earth's surface, the distance from the center of the Earth is \( R \). ### Step 2: Calculate the Potential Energy at Initial and Final Points 1. **Initial Potential Energy (PE_initial)** at height \( \frac{3R}{2} \): \[ PE_{\text{initial}} = -\frac{GMm}{\frac{3R}{2}} = -\frac{2GMm}{3R} \] 2. **Final Potential Energy (PE_final)** at the Earth's surface: \[ PE_{\text{final}} = -\frac{GMm}{R} \] ### Step 3: Calculate the Change in Potential Energy The change in potential energy as the body falls from height \( \frac{3R}{2} \) to the surface is: \[ \Delta PE = PE_{\text{final}} - PE_{\text{initial}} = \left(-\frac{GMm}{R}\right) - \left(-\frac{2GMm}{3R}\right) \] \[ \Delta PE = -\frac{GMm}{R} + \frac{2GMm}{3R} = -\frac{3GMm}{3R} + \frac{2GMm}{3R} = -\frac{GMm}{3R} \] ### Step 4: Relate Change in Potential Energy to Kinetic Energy According to the conservation of energy, the change in potential energy is equal to the kinetic energy gained: \[ \Delta PE = KE = \frac{1}{2} mv^2 \] Thus, we can write: \[ -\frac{GMm}{3R} = \frac{1}{2} mv^2 \] ### Step 5: Solve for Velocity \( v \) 1. Cancel \( m \) from both sides (assuming \( m \neq 0 \)): \[ -\frac{GM}{3R} = \frac{1}{2} v^2 \] 2. Rearranging gives: \[ v^2 = -\frac{2GM}{3R} \] 3. Taking the square root: \[ v = \sqrt{\frac{2GM}{3R}} \] ### Step 6: Relate to Escape Velocity The escape velocity \( v_e \) from the Earth's surface is given by: \[ v_e = \sqrt{\frac{2GM}{R}} \] To express \( v \) in terms of \( v_e \): \[ v = \sqrt{\frac{2GM}{3R}} = \sqrt{\frac{2GM}{R} \cdot \frac{1}{3}} = \frac{1}{\sqrt{3}} v_e \] ### Final Result Thus, the speed of the body when it hits the Earth's surface is: \[ v = \frac{1}{\sqrt{3}} v_e \]
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