NASA NTRS · 20030064976
C-SiC Composite Structures for Active Cooling
Abstract
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.
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Marshall, D. B., Cox, B. N., Berbon, M. Z., Porter, J. R.. 2003-01-01. C-SiC Composite Structures for Active Cooling. https://ntrs.nasa.gov/citations/20030064976
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