基本信息
姓名：魏祥庚
職務職稱：講師
學科：航空宇航推進理論與工程
研究方向
1.固體火箭發動機推力調節
2.組合發動機技術
學習經歷
1999年-2003年，西北工業大學，本科/學士；
2003年-2009年，西北工業大學，碩博連讀/碩士、博士
學術成就
1.魏祥庚，李江，金蔚，姜東，渦流閥式固體變推力集成原理樣機設計與實驗，固體火箭技術，2011，34（6）：703～706.
2.魏祥庚，李江，陳劍，何國強，渦流閥變推力發動機渦流室渦流結構分析，固體火箭技術，2011，34（4）：443～447.
3. WEI Xianggeng, LI Jiang, CHEN Jian, JIN Wei, Experimental investigation on throat insert’s thermal shock resistance using C/C composite in solid rocket motor,Advanced Materials Research, Vol.304,2011:169~174.
4. WEI Xianggeng, LI Jiang, CHEN Jian, DONG Hao, Ablation properties experiments of C/SiC throat-insert in operational environment of rocket engine, Advanced Materials Research, Vol.304, 2011:165~168.
5.魏祥庚，何國強，李江，陳劍，余曉京，控制流參數對渦流閥變推力固體發動機性能的影響，推進技術，2009，30（5）：571～575.
6.魏祥庚，何國強，李江，周戰鋒，非同軸式喉栓變推力發動機壓強回響分析，固體火箭技術，2009，32（4）：409～412.
7. WEI Xiang-geng, HE Guo-qiang, LI Jiang, ZHOU Zhan-feng.The Analysis on the Rising Section of Experimental Pressure in Variable Thrust pintle Solid Rocket Motor. 44rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, July 21-23, 2008. AIAA-2008-4604.
8. WEI Xiang-geng, HE Guo-qiang, LI Jiang, LIU Pei-jin, WANG Wen-bin.Experimental Rocket Motor Applied in Evaluate the Ablation Performance of Ablation Resistance Materials. 44rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, July 21-23, 2008. AIAA-2008-4887.
9. WEI Xiang-geng, HE Guo-qiang, LI Jiang, LIU Pei-jin, YU Xiao-jing. Experimental investigation on thrust modula-tion of SRM based on vortex valve. 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati，OHIO，8-11 July 2007. AIAA-2007-5827.
10.魏祥庚，何國強，李江等，渦流閥幾何參數對固體發動機推力調節特性的影響，推進技術，2007，28（4）：352～355.
11. WEI Xiang-geng, HE Guo-qiang, LIU Pei-jin, LI Xiao-zhu. Experimental research on the low vulnerability of HTPB and NEPE solid propellant. 57th International Astronautical Congress. Oct.2006. Valencia，Spain. IAC-06-C4.P.2.5.
