The abstract says they tested it in a vacuum chamber left at atmospheric pressure for some unspecified reason. I assume they did this to shield the thruster from any drafts which would have been misinterpreted as thrust, but why did they leave the vacuum chamber at atmospheric pressure? How could they then be certain that air movement caused by the differential heating of the air within the RF cavity hadn't caused the measured micro-thrust? I must be missing something because this seems to be too obvious of a potential flaw in the test.