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EFT-1 Heatshield Aerothermal Environment ReconstructionThe EFT-1 Avcoat heatshield was instrumented with 34 plugs containing multiple thermocouples in-depth with an objective being to measure the flight aerothermal environment. This paper presents a discussion of the instrumentation and the techniques used to reconstruct the heating environment from the measured in-depth temperatures. The inverse heat transfer problem algorithms, models and assumptions will be outlined, and available results will be presented.
Document ID
20150019644
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Oliver, A. Brandon
(NASA Johnson Space Center Houston, TX, United States)
Amar, Adam J.
(NASA Johnson Space Center Houston, TX, United States)
Droba, Justin
(Jacobs Technology, Inc. Houston, TX, United States)
Lessard, Victor
(NASA Langley Research Center Hampton, VA, United States)
Mahzari, Milad
(Analytical Mechanics Associates, Inc. Edwards, CA, United States)
Date Acquired
October 22, 2015
Publication Date
June 13, 2016
Subject Category
Aerodynamics
Fluid Mechanics And Thermodynamics
Report/Patent Number
JSC-CN-34558
Report Number: JSC-CN-34558
Meeting Information
Meeting: AIAA Thermophysics Conference
Location: Washington, D. C.
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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