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Results of investigations on an 0.015 scale 140a/b configuration space shuttle vehicle orbiter model (49-0) in the ltv 4 by 4-foot high speed wind tunnel (0a84)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Esparza, V. Embury, W. R. |
| Copyright Year | 1974 |
| Description | Data obtained from a wind tunnel test of an 0.015-scale 140 A/B configuration space shuttle vehicle orbiter model (49-0) are presented. Runs were conducted at Mach numbers 0.6, 0.9, 1.2, 1.6, and 2.0 and Reynolds numbers of 8.4, 9.0, 9.0, 10.9, and 13.6 million per foot respectively. Various control surface settings were investigated from angles of attack of minus 4 degrees to plus 30 degrees at fixed angles of sideslip of zero and minus 5 degrees and through angles of sideslip from minus 2 to plus 8 degrees at fixed angles of attack of zero, plus 10, plus 15, and plus 20 degrees. The purpose of the test was to define the longitudinal and lateral-directional stability and control characteristics for the updated SSV configuration. |
| File Size | 52276350 |
| Page Count | 975 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740026201 |
| Archival Resource Key | ark:/13960/t1ck35p3z |
| Language | English |
| Publisher Date | 1974-08-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Subsonic Speed Supersonic Speed Data Acquisition Wind Tunnel Tests Data Processing Transonic Speed 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 |
