Compressive mechanical properties of HTPB propellant at low, intermediate, and high strain rates-Reference-Cited by-同舟云学术

Compressive mechanical properties of HTPB propellant at low, intermediate, and high strain rates

Published:2016-02-24 Issue:23 Volume:133 Page:
ISSN:0021-8995
Container-title:Journal of Applied Polymer Science
language:en
Short-container-title:J. Appl. Polym. Sci.

Author:

Yang Long¹,Xie Kan¹,Pei Jiangfeng²,Sui Xin¹,Wang Ningfei¹

Affiliation:

1. School of Aerospace Engineering; Beijing Institute of Technology; Beijing 100081 People's Republic of China

2. Science and Technology on Combustion and Explosion Laboratory; Xi'an Modern Chemistry Research Institute; Xi'an Shanxi 710065 People's Republic of China

Funder

National Natural Science Foundation of China

Publisher

Wiley

Subject

Materials Chemistry,Polymers and Plastics,Surfaces, Coatings and Films,General Chemistry

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1002/app.43512/fullpdf

Reference41 articles.

1. Mechanical properties of propellant composite materials reinforced with ammonium perchlorate particles

2. Effects of Relaxed Modulus on the Structure Integrity of NEPE Propellant Grains during High Temperature Aging

3. Three-dimensional Structural Analysis Approach for Aging Composite Solid Propellant Grains

4. The effect of strain rate and heat developed during deformation on the stress-strain curve of plastics

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