Transverse relaxation characteristic and stress relaxation model considering molecular chains of HTPB coating based on pre-strained thermal aging-Reference-Cited by-同舟云学术

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Transverse relaxation characteristic and stress relaxation model considering molecular chains of HTPB coating based on pre-strained thermal aging

Published:2021-06 Issue:3 Volume:17 Page:821-828
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

Du Yong-qiang,Zheng Jian,Yu Gui-bo,Zhi Jian-zhuang

Funder

National Defense Pre-Research Foundation of China

Publisher

Elsevier BV

Subject

Metals and Alloys,Mechanical Engineering,Ceramics and Composites,Computational Mechanics

Reference46 articles.

1. Azide and alkyne terminated polybutadiene binders: synthesis, cross-linking, and propellant studies;Reshmi;Ind Eng Chem Res,2014

2. Experimental study on thermal decomposition kinetics of natural ageing AP/HTPB base bleed composite propellant;Zhang;Def Technol,2018

3. New developments in fracture of rubbers: predictive tools and influence of thermal aging;Nait Abdelaziz;Int J Solid Struct,2019

4. Comparison of burn rate and thermal decomposition of AP as oxidizer and PVC and HTPB as fuel binder based composite solid propellants;Manash;Def Technol,2019

5. Correlation of chemical and mechanical property changes during oxidative degradation of neoprene;Celina;Polym Degrad Stabil,2000

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1. Storage-life prediction and relationship between maximum elongation and stabilizer depletion for a composite modified double base propellant (CMDB) propellant;Mechanics of Time-Dependent Materials;2023-09-06

2. Permeability mechanism of PVC-P geomembranes based on low-field NMR technology;Geosynthetics International;2023-09-01

3. Correlation between the micro-structure and macroscopic mechanical properties of GAP-based propellant during aging;Polymer Degradation and Stability;2023-08

4. Shelf-life prediction and correlation between maximum elongation and stabilizer depletion of CMDB propellant;2023-07-10

5. The relaxation behavior of composite double-base propellants with various stabilizer content under thermal aging;Mechanics of Time-Dependent Materials;2022-10-26

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