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Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cheatham, Donald C. Eggleston, John M. Baron, Sheldon |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1960 |
| File Size | 14810928 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19890068601 |
| Archival Resource Key | ark:/13960/t1mg8bw9n |
| Language | English |
| Publisher Date | 1960-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aluminum Alloys Yield Strength Metal Fatigue Strain Rate Temperature Effects Tensile Creep Tensile Strength Tensile Stress Creep Tests High Temperature Tests Metal Sheets Rupturing Stress-strain Relationships Tensile Properties Tensile Tests Titanium Alloys Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |