Operation of an ion engine in space requires an electron source to mai
ntain the spacecraft's electrical neutrality. To neutralize exhausted
ions, a low-power, compact microwave electron source was developed. An
18-mm-diameter noncavity-type discharge chamber consisting of an L-sh
aped antenna and a magnetic circuit was developed, and electron emissi
on current of 100 mA was obtained at the power level of 10 W. maintain
ing the mass flow rate of xenon at 0.5 sccm.