NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Temperature and heat flux measurements: Challenges for high temperature aerospace applicationThe measurement of high temperatures and the influence of heat transfer data is not strictly a problem of either the high temperatures involved or the level of the heating rates to be measured at those high temperatures. It is a problem of duration during which measurements are made and the nature of the materials in which the measurements are made. Thermal measurement techniques for each application must respect and work with the unique features of that application. Six challenges in the development of measurement technology are discussed: (1) to capture the character and localized peak values within highly nonuniform heating regions; (2) to manage large volumes of thermal instrumentation in order to efficiently derive critical information; (3) to accommodate thermal sensors into practical flight structures; (4) to broaden the capabilities of thermal survey techniques to replace discrete gages in flight and on the ground; (5) to provide supporting instrumentation conduits which connect the measurement points to the thermally controlled data acquisition system; and (6) to develop a class of 'vehicle tending' thermal sensors to assure the integrity of flight vehicles in an efficient manner.
Document ID
19930004474
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Neumann, Richard D.
(Dayton Univ. Research Inst. OH, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: NASA. Langley Research Center, The 1992 NASA Langley Measurement Technology Conference: Measurement Technology for Aerospace Applications in High-Temperature Environments
Subject Category
Instrumentation And Photography
Accession Number
93N13662
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available