Publication Date:
2019-07-13
Description:
This viewgraph presentation provides an overview of research being conducted on the use of C-SiC composite structures for actively cooling rocket nozzles. Potential payoffs and design constraints are discussed. Other topics covered include: testing parameters, material selection, thermal analysis of joined tube structure, pressure containment, H2O2 combustion testing, and cooled re-entry.
Keywords:
Composite Materials
Type:
27th Annual Conference on Ceramic, Metal and Carbon Composites; Jan 27, 2003 - Jan 30, 2003; Cocoa Beach, FL; United States
Format:
text
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