The utilization of an ignition facility for a fusion propulsion experiment
is proposed. An experimental setup in the facility chamber is presented alo
ng with plasma behaviors calculated by a three-dimensional hybrid code. The
plasma instability in a magnetic nozzle is examined and the effect on thru
st efficiency is discussed. Implications of this experiment to fields other
than propulsion are also discussed. (C) 1999 Elsevier Science S.A. All rig
hts reserved.