Fabrication and Ablation Studies of 4D C/SiC Composite Nozzle Under Liquid Propulsion

Author:

Kumar Suresh12,Kumar Anil1,Mala Ramesh Babu1,Mokhasunavisu Raghvendra Rao3

Affiliation:

1. Advanced Systems Laboratory; Hyderabad 500058 India

2. Defence Materials & Stores Research and Development Establishment; Kanpur 208013 India

3. Defence Research and Development Laboratory; Hyderabad 500058 India

Publisher

Wiley

Subject

Materials Chemistry,Marketing,Condensed Matter Physics,Ceramics and Composites

Reference41 articles.

1. U. Papenburg S. Beyer H. Laube S. Walter G. Langel M. Selzer Advanced Ceramic Matrix Composites (CMC's) for Space Propulsion Systems American Institute of Aeronautics and Astronautics, 33rd Joint Propulsion Conference and Exhibit

2. B. Broquere Carbon/Carbon Nozzle Exit Cones: SEP's Experience and New Developments AIAA- 97-2674, 33rd Joint Propulsion Conference

3. R. L. Geisler The Relationship Between Solid-Propellant Formulation Variables and Nozzle Recession Rates JANNAF Rocket Nozzle Technology Subcommittee Meeting

4. L. W. Swope M. F. Berard Effects of Solid-Rocket Propellant Formulations and Exhaust-Gas Chemistries on the Erosion of Graphite Nozzles AIAA Solid Propellant Rocket Conference

5. R. Acharya K. K. Kuo Effect of Chamber Pressure & Propellant Composition on Erosion Rate of Graphite Rocket Nozzle Proceedings of 44th, AIAA Aerospace Sciences Meeting and Exhibit

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