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Data report for tests on the heat transfer effects of the 0.0175 scale rockwell international space shuttle vehicle model 22-ot in the aedc 50 inch b wind tunnel (0h4b), volume 1
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Martindale, W. Foster, T. F. Grifall, W. J. |
| Copyright Year | 1975 |
| Description | Results of wind tunnel heat transfer tests of 0.0175-scale Rockwell International Space Shuttle Vehicle configurations for orbiter alone, tank alone, and orbiter plus external tank are presented. Body flap shielding of SSME's during simulated entry was investigated. The tests were conducted at Mach 8 for thirteen Reynolds number. |
| File Size | 15365243 |
| Page Count | 655 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750010218 |
| Archival Resource Key | ark:/13960/t24b7vc99 |
| Language | English |
| Publisher Date | 1975-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance External Tanks Hypersonic Speed Wind Tunnel Tests Wind Tunnel Models Space Shuttle Orbiters Reentry Shielding Heat Transfer Environment Simulation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |