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Results of an aerodynamic force and moment investigation of an 0.015-scale configuration 3 space shuttle orbiter in the nasa/arc 3.5-foot hypersonic wind tunnel (oa58)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cleary, J. W. Dziubala, T. J. |
| Copyright Year | 1974 |
| Description | The primary objective of the test was to obtain stability and control data for the basic configuration and an alternate configuration for the Space Shuttle Orbiter. Pitch runs were made with 0 deg of sideslip at Mach numbers of 5.3, 7.3 and 10.3. Six-component force data and fuselage base pressures were recorded for each run. Shadowgraph pictures were taken at selected points. Model 420 was used for the tests. |
| File Size | 29985453 |
| Page Count | 468 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740020223 |
| Archival Resource Key | ark:/13960/t7gr1ph6x |
| Language | English |
| Publisher Date | 1974-04-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Stability Tests Pitching Moments Scale Models Hypersonic Wind Tunnels Aerodynamic Forces Space Shuttle Orbiters Sideslip Hypersonic Speed Wind Tunnel Tests Shadowgraph Photography Fuselages Base Pressure Stability Derivatives Mach Number 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 |
