TY - JOUR
T1 - Al-B alloy as a composite propellant additive
T2 - The role of B in combustion and agglomeration
AU - Jiang, Yanfeng
AU - Wen, Zhan
AU - Liu, Lu
AU - Zhan, Mingming
AU - Ao, Wen
N1 - Publisher Copyright:
© 2026 IAA
PY - 2026/5
Y1 - 2026/5
N2 - 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.
AB - 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.
KW - Agglomeration
KW - Al-B alloy
KW - Combustion
KW - Ignition
KW - Propellants
UR - https://www.scopus.com/pages/publications/105027731490
U2 - 10.1016/j.actaastro.2026.01.032
DO - 10.1016/j.actaastro.2026.01.032
M3 - 文章
AN - SCOPUS:105027731490
SN - 0094-5765
VL - 242
SP - 119
EP - 126
JO - Acta Astronautica
JF - Acta Astronautica
ER -