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A roket of mass M is launched vertically...

A roket of mass M is launched vertically upwards from trhe surface of the earth with an intial speed v . Assuming the radius of the earth to be R and negligible air resistance, the maximum height attained by the roket above the surface of the earth is

A

`( R)/((2gR)/(2v^(2)-1))`

B

`R((gR)/(2v^(2)-1))`

C

`( R)/((2gR)/(v^(2)-1))`

D

`R((2gR)/(v^(2)-1))`

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The correct Answer is:
To solve the problem of finding the maximum height attained by a rocket launched from the surface of the Earth with an initial speed \( v \), we will use the principle of conservation of energy. ### Step-by-Step Solution: 1. **Identify the Initial Energy:** The initial energy of the rocket when it is launched consists of its kinetic energy and gravitational potential energy. The kinetic energy (KE) is given by: \[ KE = \frac{1}{2} M v^2 \] The gravitational potential energy (PE) at the surface of the Earth is: \[ PE = -\frac{GMm}{R} \] where \( G \) is the gravitational constant, \( M \) is the mass of the Earth, \( m \) is the mass of the rocket, and \( R \) is the radius of the Earth. 2. **Total Initial Energy:** The total initial energy \( E_i \) at the surface of the Earth is: \[ E_i = KE + PE = \frac{1}{2} M v^2 - \frac{GMm}{R} \] 3. **Energy at Maximum Height:** At the maximum height \( h \), the rocket will momentarily come to rest, so its kinetic energy will be zero. The gravitational potential energy at height \( h \) is: \[ PE_h = -\frac{GMm}{R+h} \] Therefore, the total energy \( E_f \) at maximum height is: \[ E_f = PE_h = -\frac{GMm}{R+h} \] 4. **Apply Conservation of Energy:** According to the conservation of energy, the total initial energy must equal the total energy at maximum height: \[ E_i = E_f \] Substituting the expressions we have: \[ \frac{1}{2} M v^2 - \frac{GMm}{R} = -\frac{GMm}{R+h} \] 5. **Rearranging the Equation:** Rearranging the equation to isolate \( h \): \[ \frac{1}{2} M v^2 = -\frac{GMm}{R+h} + \frac{GMm}{R} \] \[ \frac{1}{2} M v^2 = GMm \left( \frac{1}{R} - \frac{1}{R+h} \right) \] 6. **Finding a Common Denominator:** The term \( \frac{1}{R} - \frac{1}{R+h} \) can be simplified: \[ \frac{1}{R} - \frac{1}{R+h} = \frac{(R+h) - R}{R(R+h)} = \frac{h}{R(R+h)} \] Thus, we can rewrite the energy equation as: \[ \frac{1}{2} M v^2 = GMm \cdot \frac{h}{R(R+h)} \] 7. **Solving for \( h \):** Rearranging gives: \[ h = \frac{R(R+h)}{2M v^2 / GMm} \] This leads to a quadratic equation in \( h \). Solving this quadratic equation will yield the maximum height \( h \). 8. **Final Expression:** After solving the quadratic equation, we can express the maximum height \( h \) in terms of \( R \) and \( v \).

To solve the problem of finding the maximum height attained by a rocket launched from the surface of the Earth with an initial speed \( v \), we will use the principle of conservation of energy. ### Step-by-Step Solution: 1. **Identify the Initial Energy:** The initial energy of the rocket when it is launched consists of its kinetic energy and gravitational potential energy. The kinetic energy (KE) is given by: \[ KE = \frac{1}{2} M v^2 ...
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