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Results of investigations (oa20c) on an 0.015-scale configuration 140a/b space shuttle vehicle orbiter model (49-0) in the nasa/langley research center unitary plan wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nichols, M. E. |
| Copyright Year | 1974 |
| Description | Data obtained from the wind tunnel tests of a scale model of the space shuttle orbiter configuration 140 A/B are presented. The test was conducted at Mach numbers of 2.5, 3.9, and 4.6 with Reynolds numbers from 1.25 million per foot to 5.0 million per foot. Various control surface settings were used ranging from an angle of attack range from minus 4 to plus 42 degrees at zero angle of yaw. Longitudinal stability and control characteristics of the space shuttle configuration were analyzed. |
| File Size | 6436558 |
| Page Count | 214 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740019272 |
| Archival Resource Key | ark:/13960/t9673756q |
| Language | English |
| Publisher Date | 1974-04-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Spacecraft Performance Supersonic Speed Data Acquisition Wind Tunnel Tests Aerodynamic Coefficients Wind Tunnel Models Spacecraft Stability Aerodynamic Characteristics Space Shuttle Orbiters Spacecraft Configurations 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 |
