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An investigation in the nasa msfc 14-inch trisonic wind tunnel to determine the pressure distribution over the components of a 0.004 scale version of the rockwell mcr 0074 baseline shuttle ascent configuration (ia32f), volume 3. [space shuttles - wind tunnel tests
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ramsey, P. E. |
| Copyright Year | 1975 |
| Description | For abstract, see N76-11223. |
| File Size | 27016431 |
| Page Count | 767 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760004137 |
| Archival Resource Key | ark:/13960/t52g2h87j |
| Language | English |
| Publisher Date | 1975-09-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Transducers Subsonic Speed Scale Models Space Shuttles Transonic Wind Tunnels Pressure Distribution Transonic Speed Strain Gages Tables Data Supersonic Speed Wind Tunnel Tests Spacecraft Configurations Aerothermodynamics 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 |