Abstract
A description is given of a supersonic, low density plasma tunnel employing rf excitation of the gas stream. The facility, which has been designed to be of laboratory proportions, provides clean, supersonic plasma streams at velocities up to about Mach 2. The static stream pressures available are in the range from about 0.1 to 10 Torr and jets up to 2 or 3 cm in diameter are produced. A discussion of the important design features is given and the application of this facility to several studies of supersonic plasma flow fields is described.

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