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Static aerodynamic characteristics of a three-stage rocket vehicle having various fin configurations at low subsonic mach numbers and angles of attack up to 28 deg
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1963 |
| Description | Static aerodynamic characteristics of three-stage trailblazer ii rocket vehicle determined in low turbulence pressure wind tunnel |
| File Size | 12601843 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630005431 |
| Archival Resource Key | ark:/13960/t4qk2514g |
| Language | English |
| Publisher Date | 1963-04-01 |
| Access Restriction | Open |
| Subject Keyword | Trailblazer Ii Reentry Vehicle Turbulence Static Aerodynamic Characteristics Wind Tunnel 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 |