Influence of Strain Rate on Mechanical Properties of HTPE/PCL Propellant Applying to Wide Temperature Range
Author:
Affiliation:
1. School of Materials Science and Engineering Beijing Institute of Technology Beijing 100081 China
2. Key Laboratory for Ministry of Education of High Energy Density Materials Beijing Institute of Technology Beijing 100081 China
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202000238
Reference30 articles.
1. Tensile Mechanical Properties and Constitutive Model for HTPB Propellant at Low Temperature and High Strain Rate;Wang Z.;J. Appl. Polym. Sci.,2015
2. Structural assessment of a solid propellant rocket motor: Effects of aging and damage
3. H. M. Tan The chemistry and technology of solid rocket propellant Beijing Institute of Technology Press Beijing2015 p. 136.
4. Synthesis of HTPE and Properties of HTPE Elastomers;Wang C. D.;Chin. J. Energ. Mater.,2011
5. Improvement of mechanical properties of in situ-prepared HTPE binder in propellants
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