FEASIBILITY STUDY: LATERAL IMPACT WITH STANDARD AIRCRAFT HARNESS CONFIGURATION

A series of 11 impact tests using the Daisy Decelerator was accomplished to evaluate the adequacy of restraint from lateral impact forces of up to 14 sled G using as minimal restraint, standard aircraft harness and a non-contoured seat. Standard harness would offer greater range of movement to the r...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ROTHSTEIN,Jerry D, Brown,William K
Format:	Report
Sprache:	eng
Schlagworte:	AIRCRAFT CONFIGURATIONS DECELERATION FEASIBILITY STUDIES HUMANS IMPACT TESTS Protective Equipment SAFETY BELTS Safety Engineering
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