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Experimental Tests to Characterize the Behavior and Properties of HexPly Continuous Fiber Unidirectional Composite and TuFF Discontinuous Fiber CompositeThis report summarizes test procedures for characterizing the quasistatic, room-temperature behavior of two IM7/PEKK (intermediate modulus 7/polyetherketoneketone) composite material systems: a continuous fiber (CF) carbon fiber polymer composite system from Hexcel® (Hexcel Corp.), referred to as “HUDC” (HexPly® unidirectional composite), and a discontinuous short fiber composite system provided by the University of Delaware, referred to as “TSFC” (Tailorable Universal Feedstock for Forming (TuFF) short fiber composite) or simply “TuFF.” The report also presents data obtained from analysis of the laboratory tests for the two unidirectional composites. Comparison of the mechanical properties of the TuFF fiber composite with those of the CF composite indicated that the TuFF material system has nearly equivalent (less than 15% difference) elastic moduli in all three principal material directions. Similarly, the TuFF fiber composite’s strengths under both tension and compression in the fiber direction, as well as the in-plane shear moduli, showed nearly equivalent values as compared to the CF composite. Improved transverse strength, in-plane shear strength, and both out-of-plane shear moduli were seen in the TuFF material. The TuFF material system, however, showed a significant reduction (~40%) in through-thickness tensile strength as compared to the CF material system.
Document ID
20250004329
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Ashutosh Maurya
(Arizona State University Tempe, United States)
Sateesh Pechetti
(Arizona State University Tempe, United States)
Howard Chen
(Arizona State University Tempe, United States)
Subramaniam Rajan
(Arizona State University Tempe, United States)
Javier Buenrostro
(Universities Space Research Association Columbia, United States)
J Michael Pereira
(Glenn Research Center Cleveland, United States)
Sandi G Miller
(Glenn Research Center Cleveland, United States)
Date Acquired
April 30, 2025
Publication Date
December 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-20250004329
Funding Number(s)
WBS: 966826.02.03.1655.23
INTERAGENCY: SAA3-1697
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Polymer matrix composites
Thermoplastics
Discontinuous fibers
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