Author:
Deng K.W.,Li H.Y.,Shen Z.B.,Zhang X.,Weng J.X.
Funder
National Natural Science Foundation of China
Natural Science Foundation of Hunan Province
Subject
General Engineering,General Materials Science
Reference33 articles.
1. A thermovisco-hyperelastic constitutive model of HTPB propellant with damage at intermediate strain rates;Wang;Mech. Time-dependent Mater.,2018
2. Service life prediction of AP/Al/HTPB solid rocket propellant with consideration of softening aging behavior;Walid;Chin. J. Aeronaut.,2019
3. Analysis and verification of rate related damage mechanism of HTPB composite solid propellant;Zhang;J. Propul. Technol.,2022
4. Ageing studies on AP/HTPB based composites solid propellants;Naseem;Energetic Mater. Front.,2021
5. Effect of tensile rate on mechanical properties of NEPE propellant;Guo;J. Solid Rock Technol.,2007
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