UV Spectroradiometric Output Of An F404 Turbojet Aircraft Engine

William E. Schneider; Gordon H. Spaberg

doi:10.1117/12.960720

26 September 1989 UV Spectroradiometric Output Of An F404 Turbojet Aircraft Engine

William E. Schneider, Gordon H. Spaberg

Proceedings Volume 1109, Optical Radiation Measurements II; (1989) https://doi.org/10.1117/12.960720
Event: SPIE 1989 Technical Symposium on Aerospace Sensing, 1989, Orlando, FL, United States

Abstract

Spectroradiometric measurements of the ultraviolet output of a GE F404 aircraft engine were made over the wavelength range of 200 to 320 nm. The tests were conducted at the GE Lynn, Mass. Riverworks facility in the F404 ram cell. The severe environmental conditions associated with the test cell required a special acoustical noise-proof and mechanical shock-proof enclosure for the double monochromator and UV detectors along with special long cabling to the externally located radiometer and automatic data reduction system. The tests successfully provided spectral irradiance measurements of the afterburner over the 225-320 nm wavelength range with a UV-enhanced silicon detector and over the 200-260 nm range with a PMT detector.

Citation Download Citation

William E. Schneider and Gordon H. Spaberg "UV Spectroradiometric Output Of An F404 Turbojet Aircraft Engine", Proc. SPIE 1109, Optical Radiation Measurements II, (26 September 1989); https://doi.org/10.1117/12.960720

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