Gas Permeation of Composites Subjected to Impact for Cryogenic Applications
Author:
Affiliation:
1. Mississippi State University, Mississippi State, Mississippi 39762
Funder
Mississippi Space Grant Consortium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35322
Reference29 articles.
1. KevinH. “Cyclic Cryogenic Testing of an X-33/RLV Liquid Oxygen Tank Concept,” NASA/TM-1999-209560, Hampton, VA, 1999.
2. 3.5 Design, Manufacture and Test of Cryotank Components
3. Damage trends in cryogenically cycled carbon/polymer composites
4. NettlesA.BissE. “Low Temperature Mechanical Testing of Carbon-Fiber/Epoxy-Resin Composite Materials,” NASA MSFC, NASA TP 3663, Alabama, 1996.
5. Thermally induced damage in composite laminates: Predictive methodology and experimental investigation
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