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Publishing Language: Chinese | Open Access

In-situ tomography on damage evolution of solid propellant under dynamic loading

Yongxiang YUAN1Yuexun LIU1Meng ZHAO2( )Long WANG3Chuantao HOU3Xuanjun WANG2Shengchuan WU1( )
State Key Laboratory of Rail Transit Vehicle System, Southwest Jiaotong University, Chengdu 610031, Sichuan, China
Zhijian Laboratory, Rocket Force University of Engineering, Xi’an 710025, Shaanxi, China
Key Laboratory of Science and Technology on Reliability and Environmental Engineering, Beijing Institute of Structure and Environment Engineering, Beijing 100076, China
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Abstract

Structural damages in solid propellants can lead to combustion anomalies and affect ballistic performance. Utilizing synchrotron radiation X-ray computed tomography technology and an in-situ mechanical loading test system, the macro-meso structures of nitrate ester plasticized polyether (NEPE) solid propellant were observed in-situ at compressive rates of 0.1, 1.0, and 5.0 mm/s. The compressive process employed an intermittent loading mode. With loading paused each time the preset displacement was reached to enable scanning imaging, thereby capturing the state of the propellant at specific phases during compression. Following the in-situ imaging experiment, the tomographic images of the samples were processed through projection correction and phase recovery using PITRE and PITRE_BM software, followed by image bit-depth conversion to obtain 8-bit 2D grayscale slices. Through 3D reconstruction, the typical damages and evolutionary behaviors of the solid propellant were analyzed, exploring the macroscopic deformation as well as the distribution and propagation patterns of internal micro-cracks. Results indicate that most micro-cracks nucleate and grow at the interface between filled particles and the matrix, with meso-pore evolution being rate-dependent. Unlike the continuous damage growth under tensile loading, the nucleation, growth, and closure of pores occur simultaneously during compression. Under high-rate uniaxial compressive loading, the solid propellant exhibits characteristic trumpet-shaped deformation, with spatially distributed cracks primarily located around the propellant. Macroscopic surface damage results from micro-crack propagation between near-surface particles and the matrix, with crack propagation related to the spatial location of filled particles. Transversal and axial crack propagation modes exist under dynamic compressive loading, with the transition from vertically to horizontally oriented cracks in the matrix leading to crack closure.

CLC number: O346.5; V512 Document code: A

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Cite this article:
YUAN Y, LIU Y, ZHAO M, et al. In-situ tomography on damage evolution of solid propellant under dynamic loading. Explosion and Shock Waves, 2025, 45(7). https://doi.org/10.11883/bzycj-2024-0315

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Received: 29 August 2024
Revised: 09 January 2025
Published: 05 July 2025
© 2025 Editorial Office of Explosion and Shock Waves

This is an open access article under the CC BY-NC license (https://creativecommons.org/licenses/by-nc/4.0/)