Composite Overwrapped Pressure Vessels (COPV): Flight Rationale for the Space Shuttle Program
Author:
Affiliation:
1. The Boeing Company
2. Georgia Institute of Technology
3. Cornell University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-7363
Reference10 articles.
1. GehmanJr.,H.W.,ColumbiaSpaceShuttle:AccidentInvestigationBoard,Report,Vol.1,2003.
2. Prediction of Long-Term Failure in Kevlar 49 Composites
3. Use of Raman Spectroscopy and Delta Volumes to Assess Stress Gradients in Large Kevlar/Epoxy COPVs
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2. Hypervelocity impact testing of a pressurized composite overwrapped pressure vessel and comparison to numerical analysis;Procedia Engineering;2017
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