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Results of an investigation of the 0.003-scale space shuttle external tank msfc model 460 in the nasa/msfc 14 x 14-inch trisonic wind tunnel to determine static pressure distributions during reentry (ta2f), volume 5
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ramsey, P. E. Winkler, G. W. |
| Copyright Year | 1975 |
| File Size | 14957973 |
| Page Count | 256 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760009046 |
| Archival Resource Key | ark:/13960/t2b901w0m |
| Language | English |
| Publisher Date | 1975-11-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance External Tanks Supersonic Speed Scale Models Space Shuttles Wind Tunnel Tests Pressure Distribution Wind Tunnel Models Atmospheric Entry 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 |