Effusion Cooled CMC Rocket Combustion Chamber
Author:
Affiliation:
1. DLR Institute of Structures and Design
2. DLR Institute for Space Propulsion
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3229
Reference19 articles.
1. Lezuo, Michael K, Wärmetransport in H2-transpirativ gekühlten Brennkammerkomponenten, Ph.D. thesis,RWTH Aachen, Oktober 1998.
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