The total mechanical energy is calculated as:
\( \text{Total Mechanical Energy} = \frac{PE}{2} \left( \frac{R_e}{20} \right) = 318.5 \)
The mechanical energy at the Earth's surface is:
\( \text{ME on surface of Earth} = - \frac{GMm}{R_e} \quad (\text{KE on surface} = 0) \)
The mechanical energy at a specific altitude is:
\( \text{ME at altitude} = - \frac{GMm}{R_e + \frac{R_e}{20}} = - \frac{20GMm}{2 \times 21R_e} \)
This simplifies to:
\( \text{ME at altitude} = - \frac{10GMm}{21R_e} \)
The change in total mechanical energy is determined by:
\( \text{Change in Total M.E.} = E_f - E_i \)
Substituting the values yields:
\( \text{Change in Total M.E.} = \frac{10GMm}{21R_e} - \frac{GMm}{R_e} = \frac{-10GMm + 21GMm}{21R_e} = \frac{11GMm}{21R_e} \)
Therefore, the result is:
\( x = 11 \)
The height from Earth's surface at which acceleration due to gravity becomes \(\frac{g}{4}\) is \(\_\_\)? (Where \(g\) is the acceleration due to gravity on the surface of the Earth and \(R\) is the radius of the Earth.)