Abstract:
The gain at the 10.6-μ wavelength was measured in a supersonic jet in which a stream of argon and atomic deuterium was mixed with ozone and carbon dioxide. The atomic deuterium was formed by thermal dissociation behind a reflected shock wave and flowed out through a supersonic nozzle at whose edge the ozone and carbon dioxide were mixed in. A change in the ejector design, from that used previously, resulted in a considerable increase in the measured gain. The achievement of a gain of 2.1 m–1 is reported.
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