Primary requirements of crashworthy seats and factors to consider such as occupant retention, body position, and absence of obstructions; factors for establishing design criteria for crash-worthy seats involving human decelerative limits; results of crash tests conducted to evaluate effect of variables on acceleration environment in accidents involving following aircraft -- light fixed wing type of 5000 lb or less, multiengine transport type, fighter, and helicopter; tabulation of recommended design loads for seats and restraint systems.
Review of crashworthy seat design principles
SAE -- Paper
SAE Meeting ; 1964 Seats
1964
9 pages
Aufsatz (Konferenz)
Englisch
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