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Al-B alloy as a composite propellant additive: The role of B in combustion and agglomeration

  • Yanfeng Jiang
  • , Zhan Wen
  • , Lu Liu
  • , Mingming Zhan
  • , Wen Ao
  • Northwestern Polytechnical University Xian
  • Hubei Institute of Aerospace Chemotechnology

科研成果: 期刊稿件文章同行评审

2 引用 (Scopus)

摘要

An experimental investigation was conducted to examine the effects of Al-B alloy additives on the ignition, combustion, and agglomeration characteristics of composite propellants. The properties of four Al-B alloys with different B contents (5 %, 20 %, and 50 % B) were comparatively evaluated against pure Al powder using Thermogravimetric-Differential Scanning Calorimetry, ignition research by CO2 laser, combustion experiments under high-pressure, Scanning Electron Microscopy, and X-ray Diffraction. B addition markedly accelerates the oxidation of Al, increases the total heat release, and shortens ignition delay. Regarding combustion performance, Al-B alloy propellants exhibited higher burning rates, with the alloy containing 50 % B (Al/B = 1:1) showing the most pronounced improvement and a relatively low pressure exponent. In terms of agglomeration suppression, alloys with lower B content (e.g., 5 % B) effectively decreased particle size combustion products size. However, increased B content led to greater formation of B2O3 in the combustion products, whose adhesive properties promoted particle agglomeration. Considering a trade-off among ignition delay, burning rate, and agglomeration inhibition, Al-B alloy with 50 % B content demonstrates the greatest potential for enhancing the overall performance of composite propellants.

源语言英语
页(从-至)119-126
页数8
期刊Acta Astronautica
242
DOI
出版状态已出版 - 5月 2026

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