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The effect of rocket plume contamination on the optical properties of transmitting and reflecting materialsThe preliminary results of plume contamination from a 5-pound thrust single-doublet, bipropellant rocket engine on the transmittance of quartz and the reflectance of a silicon monoxide overcoated aluminum mirror are presented. Changes in quartz transmittance were found to be significant and were due to both absorption and scattering effects. Contaminant absorption effects were predominant at the short wavelengths and scattering effects were greatest in the visible wavelengths. Measured changes in mirror reflectance were due primarily to contaminant absorption. Scattering effects were found to be as much as 9 percent of the total reflected energy from the mirror. There were no noticeable chemical or erosion effects on either the quartz or the front surface mirror.
Document ID
19720004978
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jack, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Spisz, E. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Cassidy, J. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1971
Subject Category
Physics, General
Report/Patent Number
NASA-TM-X-67974
Meeting Information
Meeting: Aerospace Sci. Meeting
Location: San Diego, CA
Country: United States
Start Date: January 17, 1972
End Date: January 19, 1972
Sponsors: AIAA
Accession Number
72N12627
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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