To solve this problem, we need to find the ratio of escape velocities between Earth and a planet with given relative properties: radius and density. The escape velocity from the surface of a celestial body of mass \(M\) and radius \(R\) is given by the formula:
\(v_e = \sqrt{\frac{2GM}{R}}\)
where \(G\) is the universal gravitational constant.
The mass \(M\) of a celestial body can be expressed in terms of its volume and density \(\rho\) as:
\(M = \rho V = \rho \left(\frac{4}{3}\pi R^3\right)\)
Substituting this in the escape velocity formula, we have:
\(v_e = \sqrt{\frac{2G \cdot \rho \cdot \left(\frac{4}{3}\pi R^3\right)}{R}} = \sqrt{\frac{8 \cdot \pi \cdot G \cdot \rho \cdot R^2}{3}}\)
Now let's determine the escape velocities at Earth and the planet:
Now, let's find the ratio of escape velocities:
\(\text{Ratio} = \frac{v_e}{v_p} = \frac{v_e}{4v_e} = \frac{1}{4}\)
There is an error in this calculation; let's revisit the correct method.
From a refined calculation, considering the radius and density impact more accurately within the root, as:
\(v_p = \sqrt{4 \cdot 2} \cdot v_e = 2\sqrt{2} \cdot v_e\)
The correct ratio should be:
\(\text{Ratio} = \frac{v_e}{v_p} = \frac{1}{2\sqrt{2}}\)
Hence, the correct ratio is \(1 : 2\sqrt{2}\).