To solve this problem we will use the Newtonian theory that describes the escape velocity of a body of a planet as:
[tex]v_e = \sqrt{\frac{2GM}{r}}[/tex]
Where,
G = Gravitational Universal Constant
M = Mass of Asteroid
r = Radius
Our values are given as,
[tex]M = 3.5*10^{16}kg[/tex]
[tex]r = 8.8*10^3m[/tex]
Replacing we have,
[tex]v_e = \sqrt{\frac{2(6.67*10^{-11})(3.5*10^{16})}{8.8*10^3}}[/tex]
[tex]v_e = 23.03m/s[/tex]
Therefore the correct answer is C.