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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 5
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hawthorne, P. J. |
| Copyright Year | 1976 |
| Description | Data obtained in wind tunnel test OA148 are presented. The objectives of the test series were to: (1) obtain pressure distributions, forces and moments over the vehicle 5 orbiter in the thermal area energy management (TAEM) and approach phases of flight; (2) obtain elevon and rudder hinge moments in the TAEM and approach phases of flight; (3) obtain body flap and elevon loads for verification of loads balancing with integrated pressure distributions; and (4) obtain pressure distributions near the short OMS pods in the high subsonic, transonic and low supersonic Mach number regimes. |
| File Size | 32203685 |
| Page Count | 694 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760023177 |
| Archival Resource Key | ark:/13960/t49p7ts4d |
| 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 Supersonic Speed Moment Distribution Wind Tunnel Tests Fuselages 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 |
