Ablation characteristics of a 4D carbon/carbon composite under a high flux of combustion products with a high content of particulate alumina in a solid rocket motor

Author:

Liu Yang,Pei Jing-qiu,Li Jiang,He Guo-qiang

Publisher

Elsevier BV

Subject

General Materials Science,Materials Science (miscellaneous)

Reference22 articles.

1. Liggett ND, Menon S. Simulation of nozzle erosion process in a solid propellant rocket motor [C]. 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper: 2007.

2. Throat materials for solid rocket motors [J];Guiming;Journal of Solid Rocket Technology,1998

3. Ablative erosion performance of four thermal protection composite materials[J];Feng;Aerospace Materials & Technology,2001

4. Pattern surface measure and ablation analysis for C/C composite material[J];Yu;Aerospace Materials & Technology,2003

5. Andrew C, Eric B, Ragini A, et al. Design of a solid rocket motor for characterization of submerged nozzle erosion[C]. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: American Institute of Aeronautics and Astronautics 2008.

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