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Discharge stabilization studies of CO laser gas mixtures in quasi-steady supersonic flow

Technical Report ·
OSTI ID:7094584
Experiments were conducted to study the applicability of a double discharge stabilization scheme in conditions appropriate for high energy CO lasers in supersonic flows. A Ludwieg tube impulse flow facility and a ballasted capacitor bank provided essentially steady flow and discharge conditions (d.c.) for times longer than ten electrode length-flow transit times. Steady, arc-free, volume discharges were produced in a Mach 3 test cavity using an auxiliary discharge to stabilize the main discharge in N/sub 2/ and He/CO mixture. A signigicant result is the lack of observed plasma E/N changes in response to auxiliary discharge current changes. Also, where glow discharges were obtained, the energy loading achieved was very much less than the threshold level required for laser operation.
Research Organization:
National Aeronautics and Space Administration, Moffett Field, CA (USA). Ames Research Center
OSTI ID:
7094584
Report Number(s):
N-77-20428; NASA-TM-X-73201; A-6897
Country of Publication:
United States
Language:
English

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