Thermochemical Erosion of Hafnium Carbide Modified Carbon/Carbon Composite Throat in a Small Solid Rocket Motor

2011 ◽  
Vol 26 (4) ◽  
pp. 427-432 ◽  
Author(s):  
Xue-Tao SHEN ◽  
Ke-Zhi LI ◽  
He-Jun LI ◽  
Tao FENG ◽  
Lei-Lei ZHANG ◽  
...  
Carbon ◽  
2012 ◽  
Vol 50 (4) ◽  
pp. 1554-1562 ◽  
Author(s):  
Li-na Peng ◽  
Guo-qiang He ◽  
Jiang Li ◽  
Lei Wang ◽  
Fei Qin

Carbon ◽  
2011 ◽  
Vol 49 (4) ◽  
pp. 1208-1215 ◽  
Author(s):  
Ke-Zhi Li ◽  
Xue-Tao Shen ◽  
He-Jun Li ◽  
Shou-Yang Zhang ◽  
Tao Feng ◽  
...  

2011 ◽  
Vol 19 (3-4) ◽  
pp. 237-245 ◽  
Author(s):  
Jian Yin ◽  
Hongbo B. Zhang ◽  
Xiang Xiong ◽  
Jinlv L. Zuo ◽  
Baiyun Y. Huang

Author(s):  
Wei-Hua Hui ◽  
Fu-Ting Bao ◽  
Xiang-Geng Wei ◽  
Yang Liu

AbstractIn this paper, a new measuring method of ablation rate was proposed based on X-ray three-dimensional (3D) reconstruction. The ablation of 4-direction carbon/carbon composite nozzles was investigated in the combustion environment of a solid rocket motor, and the macroscopic ablation and linear recession rate were studied through the X-ray 3D reconstruction method. The results showed that the maximum relative error of the X-ray 3D reconstruction was 0.0576%, which met the minimum accuracy of the ablation analysis; along the nozzle axial direction, from convergence segment, throat to expansion segment, the ablation gradually weakened; in terms of defect ablation, the middle ablation was weak, while the ablation in both sides was more serious. In a word, the proposed reconstruction method based on X-ray about C/C nozzle ablation can construct a clear model of ablative nozzle which characterizes the details about micro-cracks, deposition, pores and surface to analyze ablation, so that this method can create the ablation curve in any surface clearly.


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