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Orbiter Entry Aerodynamics Flight Testing: STS-119 and STS-125NASA has performed entry flight testing related to boundary layer transition and turbulent heating environments during 2009. Two projects are involved in implementing the activities and acquiring flight data: 1) Orbiter BLT Flight Experiment during STS-119; and 2) Hypersonic Thermodynamic Infrared Measurements (HYTHIRM) during STS-119 and STS-125. Orbiter BLT FE has implemented tile surface thermocouples in order to provide in-situ data downstream of a fixed geometry tile protuberance. HYTHIRM has developed a framework of mission planning and aircraft based telescopic infrared measurements to provide quantitative surface temperature distributions.
Document ID
20090024799
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Campbell, Charles H.
(NASA Johnson Space Center Houston, TX, United States)
Saucedo, Luis
(NASA Johnson Space Center Houston, TX, United States)
Kinder, Jerry
(Boeing Aerospace Co. Huntington Beach, CA, United States)
Horvath, Thomas J.
(NASA Langley Research Center Hampton, VA, United States)
Tomek, Deborah
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
June 18, 2009
Subject Category
Aerodynamics
Report/Patent Number
JSC-CN-18475
Meeting Information
Meeting: AIAA Transition Study Group Open Forum
Location: Texas
Country: United States
Start Date: June 21, 2009
End Date: June 25, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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