Effect of pre-strain during ageing on the maximum elongation of composite solid propellants and its modelling
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- 作者：Dongmo Zhou ; Xiangyang Liu ; liuxy@bit.edu.cn" class="auth_mail" title="E-mail the corresponding author ; Xin Sui ; Zhijun Wei ; Ningfei Wang
- 关键词：Composite solid propellants ; Pre-strain ; Maximum elongation ; Physical tension ; Chemical ageing
- 刊名：Polymer Testing
- 出版年：2016
- 出版时间：April 2016
- 年：2016
- 卷：50
- 期：Complete
- 页码：200-207
- 全文大小：1203 K
文摘
In this study, the effects of accelerated ageing under pre-strain on the maximum elongation of composite solid propellants were investigated. The maximum elongation of aged composite solid propellants at different ageing times, temperatures and pre-strains were determined. An ageing model was developed to analyse the effects of pre-strain and temperature on model parameters. Results show that pre-strain can increase the maximum elongation significantly during accelerated ageing, and the increasing amplitude exhibits a linear relationship with ageing temperature and pre-strain. The physical tension effect caused by pre-strain is a cumulative effect of the stress on samples and shows obvious characteristics of stress relaxation. The relaxation time is independent of pre-strain and exhibits an exponential relationship with ageing temperature. The effect of pre-strain on chemical ageing is related to a critical temperature TC. For the HTPB propellant investigated in this study, the TC is between 65 °C and 70 °C. When the ageing temperature is below TC, pre-strains have almost no effect on the ageing rate constant for maximum elongation kε; however, at temperatures above TC, they may promote chain scission reactions and decrease kε.