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
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
收藏
页码:553 / 557
相关论文
共 50 条
  • [1] Type Ⅰ Failure Temperature‑dependent Properties of HTPB Propellant/Liner Interface
    Ding, Wu
    Xu, Jin‑sheng
    Zhou, Chang‑sheng
    Wang, Ting‑yu
    Hou, Yu‑fei
    Hanneng Cailiao/Chinese Journal of Energetic Materials, 2022, 30 (02): : 146 - 154
  • [2] In-situ Characterization and Cure Kinetics in NEPE Propellant/HTPB Liner Interface by Microscopic FT-IR
    Gui, Dayong
    Zong, Yangyang
    Ding, Sheng
    Li, Cuihua
    Zhang, Qianling
    Wang, Mingliang
    Liu, Jianhong
    Chi, Xuhui
    Ma, Xingang
    Pang, Aimin
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2017, 42 (04) : 410 - 416
  • [3] Investigation of the Failure Mechanism of HTPB/AP/Al Propellant by In-situ Uniaxial Tensile Experimentation in SEM
    van Ramshorst, Marthinus C. J.
    Di Benedetto, Giuseppe L.
    Duvalois, Willem
    Hooijmeijer, Peter A.
    van der Heijden, Antoine E. D. M.
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2016, 41 (04) : 700 - 708
  • [4] Failure assessment on a strip biaxial tension specimen for a HTPB-based propellant material
    Renganathan, K
    Rao, BN
    Jana, MK
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 1999, 24 (06) : 349 - 352
  • [5] Studies on aging of HTPB liner for NEPE propellant(I) -Effects of chemical environment on aging behavior of liner
    Chi, Xu-Hui
    Pang, Ai-Min
    Peng, Song
    Wu, Feng-Jun
    Zhu, Xue-Zhen
    Chang, Hua
    Feng, Xue-Hua
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2010, 33 (03): : 294 - 298
  • [6] Study on Interface Failure of Propellant and Liner Material with Mechanics Analysis
    Jiang, Ai Min
    Li, Gao Chun
    Tian, Ai Ping
    ADVANCED RESEARCH ON CIVIL ENGINEERING AND MATERIAL ENGINEERING, 2012, 568 : 291 - 294
  • [7] Micromechanical Behavior of HTPB Propellant Bonding Interface under Uniaxial Tensile Loading
    Pei, Shu-di
    Qiang, Hong-fu
    Wang, Xue-ren
    Wang, Jia-xiang
    Li, Shi-qi
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2022, 47 (10)
  • [8] Mesoscopic failure behavior of HTPB propellant bonding interface under multi-angle pull-and-shear loading
    Pei, Shudi
    Qiang, Hongfu
    Wang, Xueren
    Li, Shiqi
    POLYMER TESTING, 2024, 132
  • [9] Preparation of high self-healing efficient crosslink HTPB adhesive for improving debonding of propellant interface
    Tu, Jing
    Xu, Heng
    Liang, Li
    Li, Pingyun
    Guo, Xiaode
    NEW JOURNAL OF CHEMISTRY, 2020, 44 (44) : 19184 - 19191
  • [10] Multi⁃scale Damage Evolution Analysis of HTPB Propellant Based on In⁃situ Stretching
    Li Y.-Q.
    Li G.-C.
    Lin M.-L.
    Hanneng Cailiao/Chinese Journal of Energetic Materials, 2024, 32 (02): : 124 - 132