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Material Property Characterization of AS4/VRM-34 Textile LaminatesSeveral material properties (modulus, strengths, and fracture toughness) of a textile composite have been evaluated to provide input data to analytical models of Pultruded Rod Stiffened Efficient Unitized Structure (PRSEUS). The material system is based on warp-knitted preforms of AS4 carbon fibers and VRM-34 epoxy resin, which have been processed via resin infusion and oven curing. Tensile, compressive, shear, and fracture toughness properties have been measured at ambient and elevated temperatures. All specimens were tested in as-fabricated (dry) condition. Specimens were tested with and without through-thickness stitching.
Document ID
20140004378
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Grenoble, Ray W.
(NASA Langley Research Center Hampton, VA, United States)
Johnston, William M
(Science and Technology Corp. Hampton, VA, United States)
Date Acquired
May 1, 2014
Publication Date
October 1, 2013
Subject Category
Aeronautics (General)
Composite Materials
Report/Patent Number
NF1676L-16764
NASA/TM-2013-218050
L-20276
Funding Number(s)
WBS: WBS 699959.02.22.07.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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