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Shuttle reentry aerodynamic heating test
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Smith, S. D. McCormick, P. O. Pond, J. E. |
| Copyright Year | 1971 |
| Description | The research for determining the space shuttle aerothermal environment is reported. Brief summaries of the low Reynolds number windward side heating test, and the base and leeward heating and high Reynolds number heating test are included. Also discussed are streamline divergence and the resulting effect on aerodynamic heating, and a thermal analyzer program that is used in the Thermal Environment Optimization Program. |
| File Size | 5526521 |
| Page Count | 83 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720013278 |
| Archival Resource Key | ark:/13960/t48q0s37v |
| Language | English |
| Publisher Date | 1971-12-01 |
| Access Restriction | Open |
| Subject Keyword | Thermodynamics And Combustion Thermal Protection Reentry Low Visibility Space Shuttles Aerodynamic Heating Hypervelocity Wind Tunnels Heat Transfer Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
