HTPB propellant/liner adhesive interface failure behavior based on SEM in situ tension

被引：0

作者：

Yang, Ming ^{[1
]}

Li, Gao-Chun ^{[2
]}

Qiu, Xin ^{[1
]}

Jiang, Ai-Min ^{[2
]}

机构：

[1] Graduate Management Department, Naval Aeronautical and Astronautic University, Yantai,264001, China

[2] Aircraft Engineering Department, Naval Aeronautical and Astronautic University, Yantai,264001, China

来源：

Hanneng Cailiao/Chinese Journal of Energetic Materials | 2015年 / 23卷 / 06期

关键词：

Failure (mechanical) - Propellants - Deformation - Humidity control - Polybutadienes;

D O I：

10.11943/j.issn.1006-9941.2015.06.009

中图分类号：

O63 [高分子化学（高聚物）]; TQ31 [高分子化合物工业（高聚物工业）];

学科分类号：

070305 ; 0805 ; 080501 ; 080502 ; 081704 ;

摘要：

The damage process of hydroxyl-terminated polybutadiene(HTPB) propellant/liner adhesive interface was observed by scanning electron microscope(SEM)in situ tension system. The real-time SEM images of deformation and failure for interface were collected. The micro mechanism of deformation and failure of adhesive interface was analyzed combining with the macroscopic stress(σ)-strain(Ε) curve. Results show that the tensile failure process of adhesive interface can be separated into four stages: l inear interval with larger slope(0 ©, 2015, Institute of Chemical Materials, China Academy of Engineering Physics. All right reserved.

引用

页码：553 / 557

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