Potential efficiencies of open- and closed-cycle CO, supersonic, electric-discharge lasers
Computed open- and closed-cycle system efficiencies (laser power output divided by electrical power input) are presented for a CW carbon monoxide, supersonic, electric-discharge laser. Closed-system results include the compressor power required to overcome stagnation pressure losses due to supersoni...
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Veröffentlicht in: | AIAA (Am. Inst. Aeronaut. Astronaut.) J.; (United States) 1976-05, Vol.14 (5), p.614-620 |
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Format: | Artikel |
Sprache: | eng |
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Zusammenfassung: | Computed open- and closed-cycle system efficiencies (laser power output divided by electrical power input) are presented for a CW carbon monoxide, supersonic, electric-discharge laser. Closed-system results include the compressor power required to overcome stagnation pressure losses due to supersonic heat addition and a supersonic diffuser. The paper shows the effect on the system efficiencies of varying several important parameters. These parameters include: gas mixture, gas temperature, gas total temperature, gas density, total discharge energy loading, discharge efficiency, saturated gain coefficient, optical cavity size and location with respect to the discharge, and supersonic diffuser efficiency. Maximum open-cycle efficiency of 80-90% is predicted; the best closed-cycle result is 60-70%. |
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ISSN: | 0001-1452 1533-385X |
DOI: | 10.2514/3.7130 |