NASA NTRS ยท 19730000495
Integral aircraft passenger seat
Abstract
Human-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.
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Kubokawa, C. C.. 1973-12-01. Integral aircraft passenger seat. https://ntrs.nasa.gov/citations/19730000495
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