Low frequency oscillations in a stationary plasma thruster (SPT) have been
studied using optical diagnostics and numerical models. The regime of low f
requency, large amplitude current oscillations has been especially investig
ated. The current oscillations are associated with strong oscillations of t
he light emitted by the plasma in that region. A quasi-neutral hybrid model
of the plasma can reproduce these plasma oscillations and suggests that th
ey are due to an ionization instability in the exhaust region associated wi
th the depletion of neutral atoms by electron impact ionization.