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Terminal area energy management regime investigations utilizing an 0.030-scale model (47-0) of the space shuttle vehicle orbiter configuration 140a/b/c/r in the ames research center 11 x 11 foot transonic wind tunnel (oa148), volume 6
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hawthorne, P. J. |
| Copyright Year | 1976 |
| Description | Plots and tabular listings are presented for both force and pressure data for the lower wing. |
| File Size | 21866096 |
| Page Count | 677 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760023178 |
| Archival Resource Key | ark:/13960/t94795q4r |
| Language | English |
| Publisher Date | 1976-07-01 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Terminal Area Energy Management Subsonic Speed Propulsion System Performance Transonic Wind Tunnels Pressure Distribution Transonic Speed Spacecraft Landing Descent Propulsion Systems Aerodynamic Forces Space Shuttle Orbiters Wings Supersonic Speed Moment Distribution Wind Tunnel Tests 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 |