lon Thrusters NASA's Deep Space 1 and Dawn spacecraft employed ion thrusters in which xenonions withacharge of $+1.60 \times 10^{-19} \mathrm{C}$
and a mass of $2.18 \times 10^{-25} \mathrm{kg}$ are accelerated through a potential
difference of 1315 $\mathrm{V}$ . What is the speed of the xenon ions as they
exit the thruster?