I have a science project about how different propellants affect the thrust of an Ion engine. So I have 2 questions:
How can I measure the thrust of a diy ion engine? (technique or tool that I need to buy any solution is welcome)
Is there a way for me to test other propellants other than $N_2$ in the air (where to get the gases and a setup to test it)?
Any other suggestions to add value to my research is very welcome. Thanks.
The test ion engine will look something like the one shown here.