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.
Orbiter Entry Aerothermodynamics Practical Engineering and Applied Research
2009
33 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Aerodynamics , Aerodynamic heating , Aerothermodynamics , Computational fluid dynamics , Space shuttle orbiters , Atmospheric entry , Space transportation system flights , Damage assessment , Tiles , Boundary layers , Fillers , Thermal protection , Spacecraft maintenance , Flight tests , Extravehicular activity
Configuration Aerothermodynamics of Entry Vehicles
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