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Ignition of micron amorphous boron particles in CO2 with shock tube

  • Shengyu Pang
  • , Kai Pang
  • , Long Miao
  • , Yugan Liao
  • , Xiao Hou
  • , Baolu Shi
  • School of Aerospace Engineering, Beijing Institute of Technology
  • China Aerospace Science and Technology Corporation
  • Beijing Institute of Technology

科研成果: 期刊稿件文章同行评审

2 引用 (Scopus)

摘要

This study successfully ignited 11 μm amorphous boron (B) powder in a pure carbon dioxide (CO2) atmosphere using a shock tube ignition platform, providing important insights for CO2-B reaction which was generally neglected in propulsion system. The experiments were conducted at temperatures ranging from 2100 to 2900 K and 3.5 atm, focusing on the effects of temperature and CO2 concentration on the ignition characteristics. The results show that the ignition delay time decreases with increasing temperature. And the critical ignition temperature of boron was found to beyond 2100 K. The effects of CO2 concentration on the ignition delay time and critical ignition temperature were much complex. These findings provide new data on boron ignition characteristics in CO2 environments, offering valuable reference information for CO2 propulsion technologies in space exploration.

源语言英语
期刊论文编号114311
期刊Combustion and Flame
279
DOI
出版状态已出版 - 9月 2025
已对外发布

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