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Enhancement of Aviation Fuel Thermal Stability Characterization Through Application of EllipsometryASTM D3241/Jet Fuel Thermal Oxidation Tester (JFTOT) procedure, the standard method for testing thermal stability of conventional aviation turbine fuels is inherently limited due to the subjectivity in the color standard for tube deposit rating. Quantitative assessment of the physical characteristics of oxidative fuel deposits provides a more powerful method for comparing the thermal oxidation stability characteristics of fuels, especially in a research setting. We propose employing a Spectroscopic Ellipsometer to determine the film thickness and profile of oxidative fuel deposits on JFTOT heater tubes. Using JP-8 aviation fuel and following a modified ASTM D3241 testing procedure, the capabilities of the Ellipsometer will be demonstrated by measuring oxidative fuel deposit profiles for a range of different deposit characteristics. The testing completed in this report was supported by the NASA Fundamental Aeronautics Subsonics Fixed Wing Project
Document ID
20120005439
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Browne, Samuel Tucker
(NASA Glenn Research Center Cleveland, OH, United States)
Wong, Hubert
(NASA Glenn Research Center Cleveland, OH, United States)
Hinderer, Cameron Branch
(NASA Glenn Research Center Cleveland, OH, United States)
Klettlinger, Jennifer
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
March 1, 2012
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-18051
NASA/TM-2012-217404
Funding Number(s)
WBS: WBS 561581,02,08.03.11.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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