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Experimental studies of annular (HSURIA) resonators including polarization effects. Interim report

Technical Report ·
OSTI ID:6126860
A repetitively pulsed CO/sub 2/ laser facility was developed for testing annular resonators. The large-aperture device exhibits generally uniform gain over an annular region of 18-cm outer and 10-centimeter inner diameter. The half-symmetric unstable resonator with internal axicon (HSURIA) was tested at equivalent Fresnel numbers up to 4.5. This resonator design incorporates a W-axicon mirror beam compactor that transforms a cylindrical mode region into an annular mode region. Two HSURIA configurations were evaluated (1) with a rear conical mirror and (2) with a rear flat mirror in the annular leg.
Research Organization:
Aerospace Corp., El Segundo, CA (USA). Aerophysics Lab.
OSTI ID:
6126860
Report Number(s):
AD-A-089614
Country of Publication:
United States
Language:
English