While @Hobbes points out you get less momentum per atom or per unit charge for lighter ions, assuming charge is +1 and acceleration voltage is constant, that's not the whole story.
The momentum of a particle accelerated to a kinetic energy $E = qV$ is:
$$p = \sqrt{2mqV} = \sqrt{2mE}.$$
So Hydrogen atoms give $\sqrt{131} \approx 11.4$ times less impulse or "kick" per atom, or per unit charge from your high voltage supply.
However that hydrogen atoms weights 131 times less than an atom of Xenon. So per kilogram of propellant, you get $\sqrt{131} \approx 11.4$ times more impulse or "kick" per kilogram, so if everything else were equal, hydrogen would be a much higher Isp propellant than Xenon!
Hydrogen is second the most difficult atom to ionize after helium, but the difference is not huge. Starting with H2 gas, you need about 4.5 eV just to break a hydrogen molecule into two neutral atoms, plus 13.6 eV to ionize each one. Xenon is an easier gas to ionize at only 12.1 eV.
The reason ionization is important to consider for a spacecraft is because the mass of an ion engine is tied up in the power supply and plasma-confining magnets necessary to produce the high current of medium-energy electrons in the plasma that ionize the atoms during energetic collisions.
So going from xenon to hydrogen gives you over a factor of ten in Isp, and the next step would be to lower your spacecraft mass by using a low ionization potential material. That's a separate question.
reopen
vote. You can vote to reopen as well. It would be better though if you added some explanation for why you are asking. For example, you need to know the level of the vacuum and the size of the chamber and type of pumps to understand the effect on the chamber, but maybe you only want to know about the effects on the engine? By the way the@
should only be used when you are trying to send a flag to a specific user. There is a user named everyone but they have not commented yet. $\endgroup$