High-strain-rate mechanical response of HTPE propellant under SHPB impact loading
Author:
Affiliation:
1. Xi’an Modern Chemistry Research Institute, Xi’an, Shaanxi 710065, China
Funder
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0046785
Reference31 articles.
1. Structural assessment of a solid propellant rocket motor: Effects of aging and damage
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