Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking
Solid propellant is the main part of solid rocket motor (SRM). To further investigate the service life of SRM, aging of solid propellant should be concerned. The aim of this study is to propose a new aging constitutive model of solid propellant using the degree of crosslinking. The aging development...
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Format: | Article |
Language: | English |
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Wiley
2022-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2022/2700740 |
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author | Junqi Wang Huiru Cui Weili Ma |
author_facet | Junqi Wang Huiru Cui Weili Ma |
author_sort | Junqi Wang |
collection | DOAJ |
description | Solid propellant is the main part of solid rocket motor (SRM). To further investigate the service life of SRM, aging of solid propellant should be concerned. The aim of this study is to propose a new aging constitutive model of solid propellant using the degree of crosslinking. The aging development equation of viscoelastic Poisson’s ratio (VPR) and relaxation modulus are considered in establishing the model. A series accelerated aging experiments accompanied with some tensile tests are designed to verify the new model. Aging experiments show that degree of crosslinking (DCL) can be used to act as a link to facilitate the communication between chemical aging and aged mechanical parameters well. |
format | Article |
id | doaj-art-e6657e7118c34447838efc47092111d4 |
institution | Kabale University |
issn | 1687-5974 |
language | English |
publishDate | 2022-01-01 |
publisher | Wiley |
record_format | Article |
series | International Journal of Aerospace Engineering |
spelling | doaj-art-e6657e7118c34447838efc47092111d42025-02-03T01:07:36ZengWileyInternational Journal of Aerospace Engineering1687-59742022-01-01202210.1155/2022/2700740Investigation on Aging Model of Solid Propellant Using the Degree of CrosslinkingJunqi Wang0Huiru Cui1Weili Ma2School of AstronauticsCollege of Defense EngineeringSchool of ScienceSolid propellant is the main part of solid rocket motor (SRM). To further investigate the service life of SRM, aging of solid propellant should be concerned. The aim of this study is to propose a new aging constitutive model of solid propellant using the degree of crosslinking. The aging development equation of viscoelastic Poisson’s ratio (VPR) and relaxation modulus are considered in establishing the model. A series accelerated aging experiments accompanied with some tensile tests are designed to verify the new model. Aging experiments show that degree of crosslinking (DCL) can be used to act as a link to facilitate the communication between chemical aging and aged mechanical parameters well.http://dx.doi.org/10.1155/2022/2700740 |
spellingShingle | Junqi Wang Huiru Cui Weili Ma Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking International Journal of Aerospace Engineering |
title | Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking |
title_full | Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking |
title_fullStr | Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking |
title_full_unstemmed | Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking |
title_short | Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking |
title_sort | investigation on aging model of solid propellant using the degree of crosslinking |
url | http://dx.doi.org/10.1155/2022/2700740 |
work_keys_str_mv | AT junqiwang investigationonagingmodelofsolidpropellantusingthedegreeofcrosslinking AT huirucui investigationonagingmodelofsolidpropellantusingthedegreeofcrosslinking AT weilima investigationonagingmodelofsolidpropellantusingthedegreeofcrosslinking |