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Terminal area energy management regime investigations using 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 10
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hawthorne, P. J. |
| Copyright Year | 1976 |
| Description | For abstract, see Vol. 9. |
| File Size | 26794735 |
| Page Count | 888 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760023182 |
| Archival Resource Key | ark:/13960/t2b90203t |
| Language | English |
| Publisher Date | 1976-01-01 |
| 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 ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |