科研工作:

200906-201305西北工业大学航天学院讲师201306至今西北工业大学航天学院副教授 1.魏祥庚，李江，金蔚，姜东，涡流阀式固体变推力集成原理样机设计与实验，固体火箭技术，2011，34（6）：703～706.2.魏祥庚，李江，陈剑，何国强，涡流阀变推力发动机涡流室涡流结构分析，固体火箭技术，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，何国强，李江，陈剑，余晓京，控制流参数对涡流阀变推力固体发动机性能的影响，推进技术，2009，30（5）：571～575.6.魏祥庚，何国强，李江，周战锋，非同轴式喉栓变推力发动机压强响应分析，固体火箭技术，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，何国强，李江等，涡流阀几何参数对固体发动机推力调节特性的影响，推进技术，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.

教育背景:

1999年-2003年，西北工业大学，本科/学士；2003年-2009年，西北工业大学，硕博连读/硕士、博士