To solve this problem, let's first recap the concept of escape velocity.
The escape velocity (v) from the surface of a planet or celestial body is given by the formula:
v = \sqrt{\frac{2GM}{R}}
where G is the gravitational constant, M is the mass of the planet, and R is the radius of the planet.
Assuming the mass density (\rho) is the same for both the Earth and the planet, the mass (M) of a body is given by:
M = \rho \cdot \frac{4}{3}\pi R^3
For the Earth (E) and the planet (P), this becomes:
Given that R_P = 2R_E, the mass of the planet becomes:
M_P = \rho \cdot \frac{4}{3}\pi (2R_E)^3 = 8 \rho \cdot \frac{4}{3}\pi R_E^3 = 8 M_E
Thus, substituting the expression for mass back into the escape velocity formula:
Substitute M_P and R_P:
v_P = \sqrt{\frac{2G(8M_E)}{2R_E}} = \sqrt{\frac{16GM_E}{2R_E}} = \sqrt{8} \cdot \sqrt{\frac{2GM_E}{R_E}} = 2\sqrt{2} \cdot v_E
Thus, v_P = 2v_E.
Therefore, the correct option is v_P = 2v_E.
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.)