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Static stability investigation of a sounding-rocket vehicle at mach numbers from 1.50 to 4.63
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Static stability of sounding rocket at Mach numbers 1.50 to 4.63 to determine effect of body length and fin cant |
| File Size | 12458544 |
| Page Count | 79 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19670020031 |
| Archival Resource Key | ark:/13960/t0ht7cg7k |
| Language | English |
| Publisher Date | 1967-06-01 |
| Access Restriction | Open |
| Subject Keyword | Static Stability Body Measurement Fin Sounding Rocket 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 |