Li Xintian*, Tian Hui, Yu Nanjia, Cai Guobiao. Experimental investigation of fuel regression rate in HTPB based lab-scale hybrid rocket motor[A]. 64th International Astronautical Congress[C], IAC-13,C4,P,23.p1.x19724. （EI Number: 20143117992478）

Date:2022-04-17 clicks:

Translation or Not:no

Pre One:李新田，曾鹏，田辉，蔡国飙．固液火箭发动机试验瞬时燃速分析方法[J]．推进技术，2012，33（2）：211-215．（EI Number：20122515137840） Next One:Li Xintian*, Tian Hui, Zeng Peng, Yu Nanjia, Cai Guobiao. Three-dimensional numerical simulation of the flow field in hybrid rocket motor with wagon-wheel fuel grain[A]. 63rd International Astronautical Congress[C], IAC-12, C4,2,19,x13996. （EI Number: 20133716731415）