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Infrared Observations of the Orion Capsule During EFT-1 Hypersonic ReentryHigh-resolution infrared observations of the Orion capsule during its atmospheric reentry on December 5, 2015 were made from a US Navy NP-3D. This aircraft, equipped with a long-range optical sensor system, tracked the capsule from Mach 10 to 7 from a distance of approximately 60 nmi. Global surface temperatures of the capsule's thermal heatshield were derived from near infrared intensity measurements. The global surface temperature measurements complemented onboard instrumentation and were invaluable to the interpretation of the in-depth thermocouple measurements which rely on inverse heat transfer methods and material response codes to infer the desired surface temperature from the sub-surface measurements. The full paper will address the motivations behind the NASA Engineering Safety Center sponsored observation and highlight premission planning processes with an emphasis on aircraft placement, optimal instrument configuration and sensor calibrations. Critical aspects of mission operations coordinated from the NASA Johnson Spaceflight Center and integration with the JSC Flight Test Management Office will be discussed. A summary of the imagery that was obtained and processed to global surface temperature will be presented. At the capsule's point of closest approach relative to the imaging system, the spatial resolution was estimated to be approximately 15-inches per pixel and was sufficient to identify localized temperature increases associated with compression pad support hardware on the heatshield. The full paper will discuss the synergy of the quantitative imagery derived temperature maps with in-situ thermocouple measurements. Comparison of limited onboard surface thermocouple data to the image derived surface temperature will be presented. The two complimentary measurements serve as an example of the effective leveraging of resources to advance the understanding of high Mach number environments associated with an ablated heatshield and provide unique data for the validation of design tools and numerical flight simulation techniques. Collaborative opportunities and technology investments in support of planned observations of NASA's next Orion flight test in 2018 will be explored in the full manuscript.
Document ID
20160010019
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Horvath, Thomas J.
(NASA Langley Research Center Hampton, VA, United States)
Rufer, Shann J.
(NASA Langley Research Center Hampton, VA, United States)
Schuster, David M.
(NASA Langley Research Center Hampton, VA, United States)
Mendeck, Gavin F.
(NASA Johnson Space Center Houston, TX, United States)
Oliver, A. Brandon
(NASA Johnson Space Center Houston, TX, United States)
Schwartz, Richard J.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Verstynen, Harry A.
(Unisys Corp. Hampton, VA, United States)
Mercer, C. David
(Stinger Ghaffarian Technologies, Inc. Hampton, VA, United States)
Tack, Steven
(Naval Air Warfare Center Point Mugo, CA, United States)
Ingram, Ben
(Naval Air Warfare Center Point Mugo, CA, United States)
Spisz, Thomas S.
(Johns Hopkins Univ. Laurel, MD, United States)
Taylor, Jeff C.
(Johns Hopkins Univ. Laurel, MD, United States)
Gibson, David M.
(Johns Hopkins Univ. Laurel, MD, United States)
Osei-Wusu, Kwame
(Johns Hopkins Univ. Laurel, MD, United States)
Kennerly, Steve
(Johns Hopkins Univ. Laurel, MD, United States)
Bush, Brett
(Photon Research Associates, Inc. San Diego, CA, United States)
Date Acquired
August 3, 2016
Publication Date
June 13, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Instrumentation And Photography
Report/Patent Number
NF1676L-21462
Report Number: NF1676L-21462
Meeting Information
Meeting: AIAA Aviation and Aeronautics Forum and Exposition
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 432938.11.01.07.43.40.05
Distribution Limits
Public
Copyright
Public Use Permitted.
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