DocumentCode
2903091
Title
Notes on the use of fusible temperature indicators to bound the temperature of hot graphite in the NAVSWC hypervelocity wind tunnel facility
Author
Metzger, Michael A.
Author_Institution
US Naval Surface Warfare Center, Silver Spring, MD, USA
fYear
1991
fDate
27-31 Oct 1991
Firstpage
113
Lastpage
122
Abstract
Temperature sensors, which indicate by melting whether or not a particular temperature level has been reached, were used to determine upper and lower bounds on the peak operating temperatures of a clamping fixture that is made of graphite. The clamp secures an electrically powered carbon-carbon heating element to its graphite support base in a pressure vessel that is part of the hypervelocity wind tunnel located at the US Naval Surface Warfare Center in Silver Spring, Maryland. During wind tunnel testing the clamp was exposed to an extremely hostile environment that included: temperatures to 3700°C (6700°F), intense thermal radiation, pressure to 22500 psi, hot chemically reactive carbon and carbon vapor, electrified parts, stray electromagnetic fields, and an intense aerodynamic loading
Keywords
chemical reactions; detectors; electromagnetic compatibility; graphite; pressure vessels; temperature measurement; wind tunnels; 22500 psi; 3700 C; Silver Spring; US Navy; aerodynamic loading; aerospace test facility; clamping fixture; electrified parts; fusible temperature indicators; graphite support; hot chemically reactive C; hot graphite; hypervelocity wind tunnel; military systems; peak operating temperatures; pressure vessel; stray electromagnetic fields; temperature level; temperature sensor; thermal radiation; Chemicals; Clamps; Electromagnetic radiation; Fixtures; Resistance heating; Silver; Springs; Temperature sensors; Testing; Thermal loading;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on
Conference_Location
Rockville, MD
Type
conf
DOI
10.1109/ICIASF.1991.186232
Filename
186232
Link To Document