The escape velocity from a celestial body is given by the formula:
\(v_e = \sqrt{\dfrac{2GM}{R}}\)
where
Given that the escape velocity from the Earth's surface is \(11.2\, \text{km/s}\), we are to find the new escape velocity if the Earth's mass becomes twice its present value (\(2M\)) and its radius becomes half (\(\dfrac{R}{2}\)).
Substituting these new values in the escape velocity formula, we have:
\(v'_e = \sqrt{\dfrac{2G(2M)}{\dfrac{R}{2}}} = \sqrt{\dfrac{4GM}{\dfrac{R}{2}}} = \sqrt{\dfrac{8GM}{R}}\)
Since the original escape velocity is:
\(v_e = \sqrt{\dfrac{2GM}{R}} = 11.2\, \text{km/s}\)
Comparing the two expressions, we find:
\(v'_e = \sqrt{4} \times v_e = 2 \times 11.2 = 22.4\, \text{km/s}\)
Therefore, if the Earth's mass were to double and its radius halved, the escape velocity would become \(22.4\, \text{km/s}\). Thus, the correct answer is \(22.4\, \text{km/s}\).
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.)