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Structural considerations of inflatable reentry vehicles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1960 |
| Description | The state of the design art for inflated structures applicable to reentry vehicles is discussed. Included are material properties, calculations of buckling and collapse loads, and calculations of deflections and vibration frequencies. A new theory for the analysis of inflated plates is presented and compared with experiment. |
| File Size | 744120 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19980228194 |
| Archival Resource Key | ark:/13960/t2b900d98 |
| Language | English |
| Publisher Date | 1960-09-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance 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 |