Answer:
Option C
Explanation:
We know that the escape velocity of a particle from the surface of a planet is given by
$v_{e}=\sqrt{\frac{2GM}{R}}=\sqrt{\frac{2gR^{2}}{R}}$ [ $\because GM= gR^{2}$]
$=\sqrt{2gR}$
where, g= acceleration due to gravity, and R= radius of the planet
Given, the velocity at equator , $v_{E}= V$
and acceleration due to gravity at equator
$g_{E}= \frac{1}{3}g_{p}$
$\therefore$ $g_{p}= 3 g_{E}$.........(i)
The escape velocity of a particle at equator,
$V_{E}=\sqrt{2g_{E}R}$ ..........(ii)
and at poles,
$V_{P}=\sqrt{2g_{P}R}$
$=\sqrt{2\times 3g_{E}R}=\sqrt{3}\sqrt{2g_{E}R}$ [From Eq.(i)]
$=\sqrt{3}V_{E}$ [From Eq.(ii)]
= $\sqrt {3}$ v [ $\because v_{E}=V$]
Hence, $\sqrt{3}$ v is the escape velocity for a particle at the pole of this planet.