Volume 133, Issue 23
Article

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

Long Yang

Long Yang

School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081 People's Republic of China

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Kan Xie

Corresponding Author

Kan Xie

School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081 People's Republic of China

Correspondence to: K. Xie (E-mail: [email protected])Search for more papers by this author
Jiangfeng Pei

Jiangfeng Pei

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

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Xin Sui

Xin Sui

School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081 People's Republic of China

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Ningfei Wang

Ningfei Wang

School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081 People's Republic of China

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First published: 24 February 2016
Citations: 29

ABSTRACT

Low, intermediate, and high strain rate compression testing (1.7 × 10−4 to 2500 s−1) of the hydroxyl-terminated polybutadiene (HTPB) propellant at room temperature, were performed using a universal testing machine, a hydraulic testing machine, and a split Hopkinson pressure bar (SHPB), respectively. Results show that the stress linearly increases with strain at each condition; the increasing trend of stress at a given strain with the logarithm of strain rate changes from a linear to an exponential form at 1 s−1. By combining these characteristics, we propose a rate-dependent constitutive model which is a linearly elastic component as a base model, then multiplied by a rate-dependent component. Comparison of model with experimental data shows that it can characterize the compressive mechanical properties of HTPB propellant at strain rates from 1.7 × 10−4 to 2500 s−1. © 2016 Wiley Periodicals, Inc. J. Appl. Polym. Sci. 2016, 133, 43512.

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