Infrared Imagery of the Space Shuttle at Hypersonic Entry Conditions
Author:
Affiliation:
1. The Aerospace Corporation
2. George Washington University
3. NASA Langley Research Center
4. NASA Langley
5. Swales Aerospace Incorporated
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-636
Reference12 articles.
1. Shuttle Orbiter Fuselage Global Temperature Measurements from Infrared Images at Hypersonic Speeds
2. The Shuttle Infrared Leeside Temperature Sensing (SILTS) experiment
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1. Advancing Supersonic Retro-Propulsion Technology Readiness: Infrared Observations of the SpaceX Falcon 9 First Stage;AIAA SPACE and Astronautics Forum and Exposition;2017-09-12
2. Application of a Near Infrared Imaging System for Thermographic Imaging of the Space Shuttle during Hypersonic Re-Entry;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
3. The Hythirm Project: Flight Thermography of the Space Shuttle During Hypersonic Re-Entry;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
4. Infrared Imaging of Boundary Layer Transition Flight Experiments;40th Thermophysics Conference;2008-06-15
5. Orbiter Entry Boundary Layer Flight Testing;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07
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