Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking

Author:

Wang Junqi1ORCID,Cui Huiru2ORCID,Ma Weili3ORCID

Affiliation:

1. School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China

2. College of Defense Engineering, Army Engineering University of PLA, Nanjing 210007, China

3. School of Science, Chang’an University, Xi’an 410073, China

Abstract

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.

Funder

Natural Science Foundation of Jiangsu Province

Publisher

Hindawi Limited

Subject

Aerospace Engineering

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