To determine the escape velocity on the moon relative to the given escape velocity on the planet \(v\), we will use the escape velocity formula: \(v_{\text{escape}} = \sqrt{\frac{2GM}{R}}\), where \(G\) is the gravitational constant, \(M\) is the mass of the celestial body, and \(R\) is its radius.
We are provided with the following information:
Let the planet's mass be \(M\) and its radius be \(R\). Then:
The escape velocity on the planet is \(v = \sqrt{\frac{2GM}{R}}\).
The escape velocity on the moon, \(v_{\text{moon}}\), is calculated as follows:
\(v_{\text{moon}} = \sqrt{\frac{2G \cdot M_{\text{moon}}}{R_{\text{moon}}}} = \sqrt{\frac{2G \cdot \frac{M}{144}}{\frac{R}{16}}}\)
Simplifying this expression:
\(v_{\text{moon}} = \sqrt{\frac{2G \cdot M}{144 \cdot \frac{R}{16}}} = \sqrt{\frac{2G \cdot M \cdot 16}{144 \cdot R}} = \sqrt{\frac{16}{144}} \cdot \sqrt{\frac{2G \cdot M}{R}}\)
\(v_{\text{moon}} = \frac{1}{3} \cdot \sqrt{\frac{2G \cdot M}{R}}\)
Since \(\sqrt{\frac{2G \cdot M}{R}} = v\), we can substitute this into the equation for \(v_{\text{moon}}\):
\(v_{\text{moon}} = \frac{v}{3}\)
Therefore, the escape velocity on the moon is \(\frac{v}{3}\).