Low strain rate yield characteristics and failure modes of solid composite propellant

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

Publisher

Elsevier BV

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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