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The escape velocity for a planet is v(e)...

The escape velocity for a planet is `v_(e)`. A tunnel is dug along a diameter of the planet and a small body is dropped into it at the surface. When the body reaches the centre of the planet, its speed will be

A

`v_(e)`

B

`(v_(e))/(sqrt(2))`

C

`(v_(e))/2`

D

zero

Text Solution

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The correct Answer is:
To solve the problem, we need to determine the speed of a small body when it reaches the center of a planet after being dropped from the surface through a tunnel dug along the diameter of the planet. ### Step-by-Step Solution: 1. **Understanding Escape Velocity**: The escape velocity \( v_e \) for a planet is given by the formula: \[ v_e = \sqrt{\frac{2GM}{R}} \] where \( G \) is the gravitational constant, \( M \) is the mass of the planet, and \( R \) is the radius of the planet. 2. **Potential Energy at the Surface**: The gravitational potential energy \( V_s \) at the surface of the planet is given by: \[ V_s = -\frac{GMm}{R} \] where \( m \) is the mass of the small body. 3. **Potential Energy at the Center**: The gravitational potential energy \( V_0 \) at the center of the planet is given by: \[ V_0 = -\frac{3GMm}{2R} \] 4. **Change in Potential Energy**: The change in potential energy as the body moves from the surface to the center is: \[ \Delta V = V_0 - V_s = \left(-\frac{3GMm}{2R}\right) - \left(-\frac{GMm}{R}\right) \] Simplifying this gives: \[ \Delta V = -\frac{3GMm}{2R} + \frac{GMm}{R} = -\frac{3GMm}{2R} + \frac{2GMm}{2R} = -\frac{GMm}{2R} \] 5. **Kinetic Energy at the Center**: According to the work-energy principle, the loss in potential energy equals the gain in kinetic energy. The kinetic energy \( K \) at the center is given by: \[ K = \frac{1}{2}mv^2 \] Setting the change in potential energy equal to the kinetic energy gives: \[ -\Delta V = K \implies \frac{GMm}{2R} = \frac{1}{2}mv^2 \] 6. **Solving for Speed \( v \)**: Canceling \( m \) from both sides and solving for \( v \): \[ \frac{GM}{2R} = \frac{1}{2}v^2 \implies v^2 = \frac{GM}{R} \implies v = \sqrt{\frac{GM}{R}} \] 7. **Relating to Escape Velocity**: Since we know that \( v_e^2 = \frac{2GM}{R} \), we can express \( v \) in terms of \( v_e \): \[ v = \sqrt{\frac{GM}{R}} = \sqrt{\frac{1}{2} \cdot \frac{2GM}{R}} = \frac{v_e}{\sqrt{2}} \] ### Final Answer: The speed of the body when it reaches the center of the planet is: \[ v = \frac{v_e}{\sqrt{2}} \]

To solve the problem, we need to determine the speed of a small body when it reaches the center of a planet after being dropped from the surface through a tunnel dug along the diameter of the planet. ### Step-by-Step Solution: 1. **Understanding Escape Velocity**: The escape velocity \( v_e \) for a planet is given by the formula: \[ v_e = \sqrt{\frac{2GM}{R}} ...
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Knowledge Check

  • The escape velocity for a body projected from a planet depends on

    A
    mass of the body
    B
    angle of projection
    C
    mass of the planet
    D
    radius of the body
  • The escape velocity from a planet is v_(0) . The escape velocity from a planet having twice the radius but same density will be

    A
    `0.5 v_(0)`
    B
    `v_(0)`
    C
    `2v_(0)`
    D
    `4v_(0)`
  • The escape velocity for a planet is v_(e) . A particle is projected from its surface with a speed v . For this particle to move as a satellite around the planet,

    A
    `(v_(e))/(2) lt v lt v_(e)`
    B
    `(v_(e))/(sqrt(2)) lt v lt v_(e)`
    C
    `v_(e) lt v lt sqrt()2v_(e)`
    D
    `(v)/(sqrt()2) lt v lt (v_(e))/(2)`
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