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Safety Engineering for Crash Injury Prevention
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English
Abstract
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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Authors
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.Also In
References
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