Evaluation of Mechanical Properties of Composite Solid Propellant by Genetic Engineering of Materials: Part A.
Author:
Affiliation:
1. College of Aerospace Science and Engineering National University of Defense Technology Deya Road, Kaifu District 410073 Changsha P.R. China
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201800385
Reference13 articles.
1. S. Y. Ho High strain-rate constitutive models for solid rocket propellants.J. Propul. Power 2002 181106–1111.
2. M. C. J. van Ramshorst G. L. Di Benedetto W. Duvalois P. A. Hooijmeijer A. E. D. M. van der Heijden Investigation of the failure mechanism of HTPB/AP/Al propellant by in-situ uniaxial tensile experimentation in SEM.Propellants Explos. Pyrotech. 2016 41 700–708.
3. L. Zhang S. Zhi Z. B. Shen Research on tensile mechanical properties and damage mechanism of composite solid propellants.Propellants Explos. Pyrotech. 2018 43 234–240.
4. S. J. Zhi F. Q. Cao Z. B. Shen G. Q. Xing J. W. Cao Parameters inversion of particle dewetting damage of composite solid propellants.J. Prop.Tech.2016 37 1977–1983. (In Chinese)
5. R. Manjari U. I. Somasundaran V. C. Joseph T. J. Sriram Structure-property relationship of HTPB-based propellants.II. Formulation tailoring for better mechanical properties.J. Appl. Polym. Sci. 1993 48 279–289.
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3. Evaluation of Mechanical Properties of Composite Solid Propellant by Genetic Engineering of Materials: Part B: Modeling of Minimum Representative Unit for Multi‐Modal Particle Packing Structure Based on Formulation of Composite Solid Propellant;Propellants, Explosives, Pyrotechnics;2021-02-10
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