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Effect of longitudinal and lateral controls on aerodynamic characteristics of a winged reentry configuration at a mach number of 1.97 and angles of attack up to approximately 90 deg
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1961 |
| Description | Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90-degrees |
| File Size | 1577123 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630004034 |
| Archival Resource Key | ark:/13960/t94794526 |
| Language | English |
| Publisher Date | 1961-02-01 |
| Access Restriction | Open |
| Subject Keyword | Longitudinal Control Reentry Vehicle Aerodynamic Characteristics Lateral Control 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 |