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A rocket of mass M is launched verticall...

A rocket of mass M is launched vertically from the surface of the earth with an initial speed `V= sqrt((gR)/(2))` . Assuming the radius of the earth to be R and negligible air resistance, the maximum height attained by the rocket above the surface of the earth is `(R)/(X)` where X is:

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To solve the problem of finding the maximum height attained by a rocket launched from the Earth's surface, we will use the principle of conservation of mechanical energy. ### Step-by-Step Solution: 1. **Identify the Given Values**: - Initial speed of the rocket, \( V = \sqrt{\frac{gR}{2}} \) - Radius of the Earth, \( R \) - Mass of the rocket, \( M \) (not required for calculations) - Gravitational acceleration at the surface of the Earth, \( g \) 2. **Write the Conservation of Energy Equation**: The total mechanical energy at the launch point (initial) is equal to the total mechanical energy at the maximum height (final). Thus, we can write: \[ U_i + K_i = U_f + K_f \] Where: - \( U_i \) = Initial potential energy - \( K_i \) = Initial kinetic energy - \( U_f \) = Final potential energy at maximum height - \( K_f \) = Final kinetic energy at maximum height (which is 0 at maximum height) 3. **Calculate Initial Potential and Kinetic Energy**: - Initial potential energy \( U_i = -\frac{GMm}{R} \) - Initial kinetic energy \( K_i = \frac{1}{2} M V^2 = \frac{1}{2} M \left( \frac{gR}{2} \right) = \frac{MgR}{4} \) 4. **Calculate Final Potential Energy**: At maximum height \( H \), the distance from the center of the Earth is \( R + H \): \[ U_f = -\frac{GMm}{R + H} \] 5. **Set Up the Energy Conservation Equation**: Substituting the energies into the conservation equation: \[ -\frac{GMm}{R} + \frac{MgR}{4} = -\frac{GMm}{R + H} \] 6. **Simplify the Equation**: Rearranging gives: \[ -\frac{GMm}{R + H} = -\frac{GMm}{R} + \frac{MgR}{4} \] Dividing through by \( GMm \) (assuming \( M \neq 0 \)): \[ -\frac{1}{R + H} = -\frac{1}{R} + \frac{gR}{4GM} \] 7. **Substituting \( g \)**: We know \( g = \frac{GM}{R^2} \), so substituting gives: \[ -\frac{1}{R + H} = -\frac{1}{R} + \frac{R}{4R^2} = -\frac{1}{R} + \frac{1}{4R} \] Simplifying further: \[ -\frac{1}{R + H} = -\frac{4}{4R} + \frac{1}{4R} = -\frac{3}{4R} \] 8. **Cross-Multiplying**: Cross-multiplying gives: \[ 4R = 3(R + H) \] Expanding and simplifying: \[ 4R = 3R + 3H \implies R = 3H \implies H = \frac{R}{3} \] 9. **Expressing in Terms of X**: The problem states that the maximum height \( H \) is given as \( \frac{R}{X} \). Thus: \[ \frac{R}{3} = \frac{R}{X} \implies X = 3 \] ### Final Answer: The value of \( X \) is \( 3 \).

To solve the problem of finding the maximum height attained by a rocket launched from the Earth's surface, we will use the principle of conservation of mechanical energy. ### Step-by-Step Solution: 1. **Identify the Given Values**: - Initial speed of the rocket, \( V = \sqrt{\frac{gR}{2}} \) - Radius of the Earth, \( R \) - Mass of the rocket, \( M \) (not required for calculations) ...
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