NASA NTRS ยท 20090020673
Orbiter Entry Aerothermodynamics Practical Engineering and Applied Research
Abstract
The contents include: 1) Organization of the Orbiter Entry Aeroheating Working Group; 2) Overview of the Principal RTF Aeroheating Tools Utilized for Tile Damage Assessment; 3) Description of the Integrated Tile Damage Assessment Team Analyses Process; 4) Space Shuttle Flight Support Process; and 5) JSC Applied Aerosciences and CFD Branch Applied Research Interests.
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Campbell, Charles H.. 2009-04-12. Orbiter Entry Aerothermodynamics Practical Engineering and Applied Research. https://ntrs.nasa.gov/citations/20090020673
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