The escape velocity (\(v_e\)) of a celestial body is the minimum velocity needed for an object to escape the gravitational influence of that body. The formula for escape velocity is given by:
\(v_e = \sqrt{\frac{2GM}{R}}\)
where:
For Earth, this escape velocity is given as \(v\), i.e.,
\(v = \sqrt{\frac{2GM_{\text{Earth}}}{R_{\text{Earth}}}}\)
Now, consider a planet with mass \(M_{\text{planet}}\) and radius \(R_{\text{planet}}\). According to the question:
The escape velocity for the planet would be:
\(v_{\text{planet}} = \sqrt{\frac{2G(9M_{\text{Earth}})}{16R_{\text{Earth}}}}\)
Simplify the equation:
\(v_{\text{planet}} = \sqrt{\frac{9}{16} \cdot \frac{2GM_{\text{Earth}}}{R_{\text{Earth}}}}\)
Since \(v = \sqrt{\frac{2GM_{\text{Earth}}}{R_{\text{Earth}}}}\), substitute for \(v\):
\(v_{\text{planet}} = \sqrt{\frac{9}{16}} \cdot v\)
\(v_{\text{planet}} = \frac{3}{4} \cdot v\)
Thus, the escape velocity of the planet is \(\frac{3v}{4}\).
Hence, the correct answer is \(\frac{3v}{4}\).