TY - JOUR
T1 - Interfacial regulation of Al-5Li alloy powders via a composite TPW coating for enhanced compatibility and performance in composite solid propellants
AU - Hu, Yanrui
AU - Wang, Shuo
AU - Fu, Hongdi
AU - Tian, Jingming
AU - Zhou, Qi
AU - Liu, Linlin
AU - Li, Xiaodong
AU - Song, Tinglu
AU - Zou, Meishuai
N1 - Publisher Copyright:
© 2026
PY - 2026/12/1
Y1 - 2026/12/1
N2 - Focusing on the issues of poor compatibility and interfacial instability of Al-Li alloy powders in composite solid propellants, this study develops a composite coating system composed of trimethyl phosphate (TMP), methoxy polyethylene glycol (mPEG), and paraffin wax (WAX) (denoted as TPW) to regulate the particle surface interface. The coating structure and composition are characterized by TEM, ToF-SIMS, and XPS. The results indicate that TPW forms a relatively continuous and uniform interfacial layer on the particle surface. This interfacial structure improves the compatibility between Al-5Li and typical propellant components, namely hydroxyl-terminated polybutadiene (HTPB) and ammonium perchlorate (AP), stabilizing the thermal decomposition behavior and improving the mechanical performance of the propellant. Meanwhile, the combustion heat of the powder does not decrease significantly after coating, and it shows excellent combustion response characteristics. With this interfacial structure in place, a practical balance can be achieved among compatibility, structural integrity, and energy output, offering a new approach for applying Al-Li alloy powders in composite propellants.
AB - Focusing on the issues of poor compatibility and interfacial instability of Al-Li alloy powders in composite solid propellants, this study develops a composite coating system composed of trimethyl phosphate (TMP), methoxy polyethylene glycol (mPEG), and paraffin wax (WAX) (denoted as TPW) to regulate the particle surface interface. The coating structure and composition are characterized by TEM, ToF-SIMS, and XPS. The results indicate that TPW forms a relatively continuous and uniform interfacial layer on the particle surface. This interfacial structure improves the compatibility between Al-5Li and typical propellant components, namely hydroxyl-terminated polybutadiene (HTPB) and ammonium perchlorate (AP), stabilizing the thermal decomposition behavior and improving the mechanical performance of the propellant. Meanwhile, the combustion heat of the powder does not decrease significantly after coating, and it shows excellent combustion response characteristics. With this interfacial structure in place, a practical balance can be achieved among compatibility, structural integrity, and energy output, offering a new approach for applying Al-Li alloy powders in composite propellants.
KW - Al-Li alloy
KW - Compatibility
KW - Composite coating
KW - Solid propellant
UR - https://www.scopus.com/pages/publications/105044767232
U2 - 10.1016/j.apsusc.2026.167821
DO - 10.1016/j.apsusc.2026.167821
M3 - Article
AN - SCOPUS:105044767232
SN - 0169-4332
VL - 748
JO - Applied Surface Science
JF - Applied Surface Science
M1 - 167821
ER -