Effects of Fiber Reinforcement Architecture on the Hygrothermal-Mechanical Performance of Polyimide Matrix Composites for Aeropropulsion Applications

A lightweight sandwich support structure, for the combustor chamber of a new generation liquid propellant rocket engine, was designed and fabricated using a polymer matrix composite (PMC) facesheet on a Ti honeycomb core. The PMC facesheet consisted of high stiffness carbon fiber, M40JB, and high te...

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Bibliographische Detailangaben

Hauptverfasser:	Shin, E. Eugene, Thesken, John C., Sutter, James K., Chuang, Kathy, Juhas, John, Veverka, Adrienne, Inghram, Linda, Papadopoulos, Demetrios, Burke, Chris, Scheiman, Dan
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Composite Materials
Online-Zugang:	Volltext bestellen
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