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An empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1966 |
| Description | Empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles |
| File Size | 5053020 |
| Page Count | 107 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660010176 |
| Archival Resource Key | ark:/13960/t7fr4mq73 |
| Language | English |
| Publisher Date | 1966-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Load Multistage Rocket Vehicle Static Loading Axisymmetric Body Load Distribution Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |