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Aerodynamic characteristics of a 60 degree swept delta-wing space shuttle orbiter at mach numbers of 2.50, 3.90, and 4.60
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Graves, E. B. |
| Copyright Year | 1972 |
| Description | Wind tunnel tests were performed to determine the static aerodynamic characteristics of a model of a 60 degree swept delta wing space shuttle orbiter. Some control effectiveness tests were included. The tests were conducted in a unitary plan wind tunnel at Mach numbers of 2.50, 3.90, and 4.60. |
| File Size | 23206970 |
| Page Count | 117 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720018347 |
| Archival Resource Key | ark:/13960/t4zh1d637 |
| Language | English |
| Publisher Date | 1972-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Delta Wings Spacecraft Control Wind Tunnel Models Aerodynamic Characteristics Space Shuttle Orbiters Spacecraft Design Spacecraft Configurations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |