Response of HTPB propellants subjected to high-pressure waterjet

Hong Tao Yu*, Qing Ming Zhang, Yuan Hang He

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

摘要

In order to investigate the ignition mechanism of HTPB propellants subjected to high pressure waterjet, different formulas were selected, the researches on the impact effects of high-pressure waterjet were carried out, and they were analyzed by using SEM and infrared spectra before and after impact. The results show that the surface morphology and composition of HTPB propellant change under the impact of high-pressure waterjet and it changes chemically, and the contents of ammonium perchlorate and ferrocene affect the chemical change greatly.

源语言英语
页(从-至)355-359
页数5
期刊Binggong Xuebao/Acta Armamentarii
32
SUPPL. 2
出版状态已出版 - 12月 2011

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引用此

Yu, H. T., Zhang, Q. M., & He, Y. H. (2011). Response of HTPB propellants subjected to high-pressure waterjet. Binggong Xuebao/Acta Armamentarii, 32(SUPPL. 2), 355-359.