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Testing of Carbon Fiber Composite Overwrapped Pressure Vessel Stress-Rupture LifetimeThis paper contains summaries of testing procedures and analysis of stress rupture life testing for two stress rupture test programs, one for Kevlar COPVs performed at Lawrence Livermore National Laboratory, and the other a joint study between NASA JSC White Sands Test Facility and the Jet Propulsion Laboratory. These will be discussed in detail including test setup and issues encountered during testing. Lessons learned from testing in these two programs will be discussed.
Document ID
20070018090
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/39869
Authors
Grimes-Ledesma, Lorie (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Phoenix, S. Leigh (Cornell Univ. Ithaca, NY, United States)
Beeson, Harold (NASA Johnson Space Center Houston, TX, United States)
Yoder, Tommy (Honeywell Technology Solutions, Inc. Las Cruces, NM, United States)
Greene, Nathaniel (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 23, 2013
Publication Date
September 17, 2006
Subject Category
Composite Materials
Meeting Information
Meeting: ASC/ASTM 21st Annual Technical Conference of the American Society for Composite
Location: Dearborn, MI
Country: United States
Start Date: September 17, 2006
End Date: September 20, 2006
Sponsors: American Society for Testing and Materials, American Society for Composites
Distribution Limits
Public
Copyright
Other
Keywords
lightweight propellant tanks
composite tanks

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