Loading...
Please wait, while we are loading the content...
Similar Documents
Results of investigations on an 0.015-scale configuration 140a/b space shuttle vehicle orbiter model (49-0) in the nasa/langley research center 8-foot transonic pressure tunnel (oa25)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nichols, M. E. |
| Copyright Year | 1974 |
| Description | Aerodynamic force and moment tests were conducted on an 0.015-scale space shuttle vehicle configuration 140A/B model (49-0) in a transonic pressure tunnel. The test was carried out at Mach numbers 0.35, 0.60, 0.80, 0.90, 0.98, and 1.20, and at Reynolds numbers ranging from 1.90 million per foot to 3.97 million per foot, depending on tunnel total pressure capability and model structural limits. The model attitude was varied in angle-of-attack from minus 2 deg to +22 deg at 0 deg and 5 deg angles of yaw, and in angle-of-sidelip from minus 5 to +10 deg at 0 deg, 7.5 deg, and 15 deg angles of pitch. The purpose of this test was to establish and verify longitudinal and lateral-directional characteristics of the 140A/B Configuration Orbiter and to determine the effects of surface deflections on vehicle performance, stability, and control. |
| File Size | 26523174 |
| Page Count | 590 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740014392 |
| Archival Resource Key | ark:/13960/t95766850 |
| Language | English |
| Publisher Date | 1974-02-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Spacecraft Performance Subsonic Speed Wind Tunnel Tests Lateral Stability Transonic Speed Wind Tunnel Models Flight Control Space Shuttle Orbiters Spacecraft Configurations Longitudinal Stability 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 |
