Evaluation of Mechanical Properties of Composite Solid Propellant by Genetic Engineering of Materials: Part A.-Reference-Cited by-同舟云学术

Evaluation of Mechanical Properties of Composite Solid Propellant by Genetic Engineering of Materials: Part A.

Published:2019-08-16 Issue:9 Volume:44 Page:1167-1174
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Prop., Explos., Pyrotech.

Author:

Zhang Wei¹,Zhou Xing¹,Bao Tong¹,Deng Lei¹,Gao Dong‐lei¹

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.

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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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