\(\frac{Rk^2}{1-k^2}\)
\(R(\frac{k}{1-k})^2\)
\(R(\frac{k}{1+k})^2\)
\(\frac{R^2k}{1+k}\)
To solve this problem, we need to calculate the maximum height reached by a particle projected with an initial velocity \( v = kV_e \) from the Earth's surface. Here, \( V_e \) is the escape velocity, and \( k < 1 \) is a given constant. We are given four options, and we need to verify which one is correct.
First, let's recall the formula for escape velocity \( V_e \):
\(V_e = \sqrt{\frac{2GM}{R}}\)
where \( G \) is the gravitational constant, \( M \) is the mass of the Earth, and \( R \) is the Earth's radius.
Now, according to the problem, the initial kinetic energy of the particle is:
\(KE_{initial} = \frac{1}{2} mv^2 = \frac{1}{2} m (kV_e)^2 = \frac{1}{2} m k^2 V_e^2\)
The potential energy at the Earth's surface is:
\(PE_{initial} = -\frac{GMm}{R}\)
At the maximum height \((h)\), the final kinetic energy is zero because the particle momentarily comes to rest, and the potential energy is:
\(PE_{final} = -\frac{GMm}{R+h}\)
By conservation of energy, the initial total energy should be equal to the final total energy:
\(\frac{1}{2} m k^2 V_e^2 - \frac{GMm}{R} = -\frac{GMm}{R+h}\)
Substituting \( V_e^2 = \frac{2GM}{R} \) into the equation:
\(\frac{1}{2} m k^2 \cdot \frac{2GM}{R} - \frac{GMm}{R} = -\frac{GMm}{R+h}\)
Simplifying further:
\(m k^2 \frac{GM}{R} - \frac{GMm}{R} = -\frac{GMm}{R+h}\)
Dividing through by \( m \), we have:
\(k^2 \frac{GM}{R} - \frac{GM}{R} = -\frac{GM}{R+h}\)
Rearranging terms gives:
\(GM \left( \frac{k^2 - 1}{R} \right) = -\frac{GM}{R+h}\)
We can cancel \( GM \) from both sides:
\(\frac{k^2 - 1}{R} = -\frac{1}{R+h}\)
Cross-multiplying yields:
\(R(k^2 - 1)(R + h) = -R^2\)
Expanding and simplifying:
\(Rk^2 - R - k^2Rh + R^2h = -R^2\)
\(R^2 - R^2k^2 = -k^2Rh + R^2h\)
Reorganize to solve for \( h \):
\(h(R^2 - k^2R) = R^2(1-k^2)\)
Finally, solve for \( h \):
\(h = \frac{Rk^2}{1-k^2}\)
Thus, the correct answer is:
\(h = \frac{Rk^2}{1-k^2}\)
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.)