Safety Engineering for Crash Injury Prevention

640600

01/01/1964

Event
SAE World Congress & Exhibition
Authors Abstract
Content
Methods of achieving crash-worthiness of aircraft in general are discussed. Specific conclusions are drawn with regard to the design loads for occupant restraint systems. A “ programmed break” concept for the fuselage of large aircraft is presented, and additional research which is needed to provide increased survival in accidents is suggested.
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DOI
https://doi.org/10.4271/640600
Pages
14
Citation
Haley, J., Turnbow, J., and Avery, J., "Safety Engineering for Crash Injury Prevention," SAE Technical Paper 640600, 1964, https://doi.org/10.4271/640600.
Additional Details
Publisher
Published
Jan 1, 1964
Product Code
640600
Content Type
Technical Paper
Language
English