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Integral aircraft passenger seatHuman-engineering approach was used to design integral seat which provides all the safety, comfort, and protective features that can possibly be afforded airline passengers. Results of dynamic impact testing indicated that seat can withstand and attenuate gravity loads of 21-g horizontal and 45-g vertical; by design, seat will withstand lateral g's as well.
Document ID
19730000495
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kubokawa, C. C.
Date Acquired
August 7, 2013
Publication Date
December 1, 1973
Subject Category
Life Sciences
Report/Patent Number
ARC-10799
Accession Number
73B10495
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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