Dual inhibition mechanism of core-shell coatings on CL-20 and HMX crystals for suppressing co-crystallization in composite propellants

The freeze-drying process successfully produced a dense polyvinylpyrrolidone (PVP) coating on the surfaces of CL-20 and HMX crystals. This PVP layer effectively inhibited the spontaneous and undesirable co-crystallization of CL-20 and HMX within propellants through a dual inhibition mechanism, and reduced sensitivity and enhanced the thermal stability of the explosives. • A dual inhibition strategy using polyvinylpyrrolidone coatings effectively suppresses hexanitrohexaazaisowurtzitane/cyclotetramethylene tetranitramine (CL-20/HMX) co-crystallization in propellant formulations. • Polyvinylpyrrolidone coatings simultaneously exhibit sacrificial dissolution in glycidyl azide polymer and a physical barrier against plasticizer dioctyl sebacate penetration, ensuring long-term structural stability. • Molecular simulations and X-ray photoelectron spectroscopy reveal strong interfacial interactions between polyvinylpyrrolidone and energetic crystals, enhancing thermal resilience and kinetic stability. • The core–shell architecture significantly reduces mechanical sensitivity (by up to 100%) and increases combustion efficiency (by up to 33%). The unintended co-crystallization of hexanitrohexaazaisowurtzitane (CL-20) and cyclotetramethylene tetranitramine (HMX) compromises the structural integrity and safety of composite propellants during long-term storage. Inspired by pharmaceutical crystallization control, this study proposes a colloidal interface engineering strategy that utilizes conformal polyvinylpyrrolidone (PVP) coatings on CL-20 and HMX crystals by freeze-drying. The coatings strategy exhibit “sacrificial dissolution” and “physical barrier” dual inhibition mechanism. PVP preferentially saturates the glycidyl azide polymer (GAP) binder through controlled dissolution, deactivating the capacity to dissolve CL-20 and HMX. Simultaneously, PVP forms a dense barrier against plasticizer dioctyl sebacate (DOS) penetration. Molecular dynamics simulations and density functional theory calculations confirmed superior PVP binding affinity to CL-20 and HMX surfaces, which is validated by X-ray photoelectron spectroscopy and atomic force microscopy. Accelerated aging tests (70 °C/30 days) demonstrated complete co-crystallization suppression in PVP-coated formulations. Thermal analysis revealed a 20-30°C increase in phase transition temperatures and enhanced activation energies, attributed to restricted molecular mobility and optimized heat dissipation. Mechanical sensitivity decreased by 50–100 %, while combustion rates increased by 18–33 %. This work bridges pharmaceutical-inspired interfacial control with energetic materials, establishing a universal methodology for stabilizing high-energy composites through kinetic control.

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Publication Details

Journal
Materials & Design
Published
2025-08-29
DOI
https://doi.org/10.1016/j.matdes.2025.114651
Citations
2
Primary Topic
Energetic Materials and Combustion
Type
article
Field-Weighted Citation Impact
1.73
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article

Dual inhibition mechanism of core-shell coatings on CL-20 and HMX crystals for suppressing co-crystallization in composite propellants

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2 citations
Materials & Design
Energetic Materials and Combustion
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article

Dual inhibition mechanism of core-shell coatings on CL-20 and HMX crystals for suppressing co-crystallization in composite propellants

Jie Li, Haobin Zhang, Shichun Li, Jinjiang Xu, Shiliang Huang, Liangbin Li, Pangangjing Zou, Yu Liu
article en
2 citations

Abstract

The freeze-drying process successfully produced a dense polyvinylpyrrolidone (PVP) coating on the surfaces of CL-20 and HMX crystals. This PVP layer effectively inhibited the spontaneous and undesirable co-crystallization of CL-20 and HMX within propellants through a dual inhibition mechanism, and reduced sensitivity and enhanced the thermal stability of the explosives. • A dual inhibition strategy using polyvinylpyrrolidone coatings effectively suppresses hexanitrohexaazaisowurtzitane/cyclotetramethylene tetranitramine (CL-20/HMX) co-crystallization in propellant formulations. • Polyvinylpyrrolidone coatings simultaneously exhibit sacrificial dissolution in glycidyl azide polymer and a physical barrier against plasticizer dioctyl sebacate penetration, ensuring long-term structural stability. • Molecular simulations and X-ray photoelectron spectroscopy reveal strong interfacial interactions between polyvinylpyrrolidone and energetic crystals, enhancing thermal resilience and kinetic stability. • The core–shell architecture significantly reduces mechanical sensitivity (by up to 100%) and increases combustion efficiency (by up to 33%). The unintended co-crystallization of hexanitrohexaazaisowurtzitane (CL-20) and cyclotetramethylene tetranitramine (HMX) compromises the structural integrity and safety of composite propellants during long-term storage. Inspired by pharmaceutical crystallization control, this study proposes a colloidal interface engineering strategy that utilizes conformal polyvinylpyrrolidone (PVP) coatings on CL-20 and HMX crystals by freeze-drying. The coatings strategy exhibit “sacrificial dissolution” and “physical barrier” dual inhibition mechanism. PVP preferentially saturates the glycidyl azide polymer (GAP) binder through controlled dissolution, deactivating the capacity to dissolve CL-20 and HMX. Simultaneously, PVP forms a dense barrier against plasticizer dioctyl sebacate (DOS) penetration. Molecular dynamics simulations and density functional theory calculations confirmed superior PVP binding affinity to CL-20 and HMX surfaces, which is validated by X-ray photoelectron spectroscopy and atomic force microscopy. Accelerated aging tests (70 °C/30 days) demonstrated complete co-crystallization suppression in PVP-coated formulations. Thermal analysis revealed a 20-30°C increase in phase transition temperatures and enhanced activation energies, attributed to restricted molecular mobility and optimized heat dissipation. Mechanical sensitivity decreased by 50–100 %, while combustion rates increased by 18–33 %. This work bridges pharmaceutical-inspired interfacial control with energetic materials, establishing a universal methodology for stabilizing high-energy composites through kinetic control.

Materials & DesignVol. 258
University of Science and Technology of China (CN), China Academy of Engineering Physics (CN)
Openalex Percentile: Top 15%
Energetic Materials and Combustion
1.73
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