Methods of achieving crashworthiness of aircraft in general are discussed; specific conclusions are drawn with regard to design loads for occupant restraint systems; "programmed break" concept for fuselage of large aircraft is presented, and additional research which is needed to provide increased survival in accidents is suggested.
Safety engineering for crash injury prevention
SAE -- Proc
Proceedings of 3rd Aerospace Reliability and Maintainability Conference ; 1964 Accident prevention
1964
14 pages
Aufsatz (Konferenz)
Englisch
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