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NASA seat experiment and occupant responsesResults of the crash test of a remotely piloted transport aircraft instrumented to measure a NASA energy-absorbing transport seat are given. Human tolerance limits to acceleration and a dynamic response index model are discussed. It was found that the acceleration levels at the rear of the airplane were quite low and were below the stroking threshold of the NASA EA-seat. Therefore, dummies in the standard and EA-seat responded approximately the same. All longitudinal accelerations were quite low for the primary impact with very low forces measured in the lap belts. The vertical (spineward) acceleration levels measured in the dummies were also relatively low and very survivable from an impact tolerance standpoint. The pilot with an 18 G peak acceleration received by far the highest vertical acceleration and could have possibly received slight spinal injury.
Document ID
19860012468
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fasanella, E. L.
(PRC Kentron, Inc. Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: NASA. Langley Research Center Full-Scale Transport Controlled Impact Demonstration
Subject Category
Structural Mechanics
Accession Number
86N21939
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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