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Aerodynamic characteristics at a mach number of 6.77 of a 9 deg cone configuration, with and without spherical afterbodies, at angles of attack up to 180 deg with various degrees of nose blunting
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1963 |
| Description | Aerodynamic characteristics at mach 6.77 of 9-deg cone, with and without spherical afterbody and nose blunting at angles of attack to 180-deg |
| File Size | 2989614 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630003686 |
| Archival Resource Key | ark:/13960/t3227n81h |
| Language | English |
| Publisher Date | 1963-03-01 |
| Access Restriction | Open |
| Subject Keyword | Afterbody Aerodynamic Characteristics Reentry Vehicle Cone Nose Hypersonic Speed Blunt Body 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 |