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Results from tests of three prototype general aviation seats
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Williams, M. S. Fasanella, E. L. |
| Copyright Year | 1982 |
| Description | Three types of energy absorbing general aviation seats were dynamically tested and evaluated for crash load attenuation. On the basis of the static and dynamic test results, it was recommended that the tubular frame seats be redesigned to initiate stroking at approximately 12 G's rather than the 20 to 25 G range. Lower density foam was recommended for the foam wedge passenger seat. |
| File Size | 11791544 |
| Page Count | 58 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820025857 |
| Archival Resource Key | ark:/13960/t7zm05q3j |
| Language | English |
| Publisher Date | 1982-08-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Foams Dynamic Tests Low Density Materials Human Factors Engineering General Aviation Aircraft Impact Loads Energy Absorption Crashworthiness Static Tests Seats 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 |
