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Ignition and Combustion Characteristics of Aluminum Hydride-Based Kerosene Propellant

  • Jiangong Zhao
  • , Chenzhuo Hao
  • , Yilun Liu
  • , Yihao Fu
  • , Wen Ao
  • Northwestern Polytechnical University Xian

科研成果: 期刊稿件文章同行评审

1 引用 (Scopus)

摘要

Aluminum hydride (AlH3) is a promising candidate for enhancing the combustion performance of liquid fuels due to its high energy density and exceptional hydrogen storage capacity. This study investigated the ignition and combustion characteristics of μ-AlH3 particles in kerosene droplets using TG-DSC analysis, high-speed imaging, laser ignition, and combustion product characterization, with comparisons to micron- and nano-aluminum powders. Results showed that the exothermic combustion of hydrogen released from AlH3 decomposition lowered the primary oxidation temperature of aluminum, leading to more intense combustion with smaller ejected particles. The particle size of kerosene droplets containing AlH3 rapidly decreases due to the escape of hydrogen. The heat released by the combustion of hydrogen significantly accelerates the combustion of droplets, and the fastest combustion rate is observed at a concentration of 1% AlH3. The combustion products of kerosene droplets containing AlH3 are smaller than those of kerosene droplets containing aluminum, indicating that their combustion efficiency is higher. A combustion model for AlH3-based kerosene droplets was developed, demonstrating less than 10% error in predicting ignition delay and burning rates. These findings provide valuable insights for the application of AlH3 in liquid fuels.

源语言英语
文章编号891
期刊Aerospace
12
10
DOI
出版状态已出版 - 10月 2025

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