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NASA Prototype All Composite Tank Cryogenic Pressure Tests to Failure with Structural Health MonitoringThis Paper will describe the results of pressurization to failure of 100 gallon composite tanks using liquid nitrogen. Advanced methods of health monitoring will be compared as will the experimental data to a finite element model. The testing is wholly under NASA including unique PZT (Lead Zirconate Titanate) based active vibration technology. Other technologies include fiber optics strain based systems including NASA AFRC technology, Acoustic Emission, Acellent smart sensor, this work is expected to lead to a practical in-Sutu system for composite tanks.
Document ID
20150018435
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Werlink, Rudolph J.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Pena, Francisco
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
September 28, 2015
Publication Date
September 1, 2015
Subject Category
Structural Mechanics
Report/Patent Number
KSC-E-DAA-TN24733
Meeting Information
Meeting: International Workshop on Structural Health Monitoring 2015
Location: Stanford, CA
Country: United States
Start Date: September 1, 2015
End Date: September 3, 2015
Sponsors: Stanford Univ.
Funding Number(s)
WBS: WBS 359615.01.02.11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
tanks
Cryogenic
health
monitoring
composite
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