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Characterization of Polymer-Coated MEMS Humidity Sensors for Flight ApplicationsUnder NASA's Aviation Safety Program (AvSP), in addition to wind velocity and temperature, water vapor is considered one key factor in determining aviation weather, which is a substantial contributor to many general aviation (GA) accidents. The conventional and reliable humidity measuring methods such as radiation reflection or absorption have relatively high cost in addition to highly specialized operating and maintenance characteristics. This paper presents characterizations of inexpensive MEMS and capacitance type humidity sensors for their potential use on aircraft. If installed, these sensors are subjected to ambient environmental conditions as well as to different chemicals and deicing fluids used on aircraft. This paper reports the effect of different deicing fluids and chemicals on these inexpensive humidity sensors.
Document ID
20050229950
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Shams, Qamar A.
(NASA Langley Research Center Hampton, VA, United States)
Burkett, Cecil G., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Daniels, Taumi S.
(NASA Langley Research Center Hampton, VA, United States)
Tsoucalas, George
(NASA Langley Research Center Hampton, VA, United States)
Comeaux, Toby
(NASA Langley Research Center Hampton, VA, United States)
Sealey, Bradley S.
(NASA Langley Research Center Hampton, VA, United States)
Fox, Melanie L.
(Christopher Newport Univ. Newport News, VA, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2005
Subject Category
Avionics And Aircraft Instrumentation
Report/Patent Number
NASA/TP-2005-213770
L-19142
Funding Number(s)
WORK_UNIT: WU 23-781-40-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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