TY - JOUR
T1 - Accelerating the Combustion of Aluminum Diboride (AlB2) Fuel with Functionalized Carbon Nanomaterials
AU - Wen, Tingrui
AU - Jiang, Yue
AU - Xu, Dunhui
AU - Han, Wang
AU - Li, Jingxuan
AU - Yu, Tao
AU - Yang, Lijun
N1 - Publisher Copyright:
© Chinese Society of Astronautics 2025.
PY - 2026/3
Y1 - 2026/3
N2 - Aluminum diboride (AlB2) has been proposed as a viable substitute for elemental boron as the fuel for boron-containing solid propellants, owing to its favorable compatibility with propellant formulations, high gravimetric heat of combustion, and the anticipated synergistic effects from boron and aluminum. Nevertheless, its practical implementation is impeded by intrinsically low energy-release rates and pronounced agglomeration. In this study, two-dimensional graphene fluoride (GF), three-dimensional polytetrafluoroethylene (PTFE), and two-dimensional graphene oxide (GO) were strategically incorporated to construct composite fuel systems capable of fully exploiting the energetic potential of AlB2. Laser-ignition experiments demonstrated that GF, GO, and PTFE all generate abundant gaseous products while markedly intensifying the combustion of AlB2, while GF exhibits better enhancing effects. Thermal analyses reveal that fluorinated additives markedly enhance the thermal oxidation characteristics of AlB2, effecting a pronounced reduction in its initial decomposition temperature. The difference in the combustion mechanism of AlB2 with GF and GO lies in the fluorine, although they both open alternative reaction pathways, GF exhibits more notable capacity to suppress agglomeration of condensed combustion products. The formulation developed and mechanisms revealed by this work could potentially advance the applications of boron-based fuels in ramjets and scramjets.
AB - Aluminum diboride (AlB2) has been proposed as a viable substitute for elemental boron as the fuel for boron-containing solid propellants, owing to its favorable compatibility with propellant formulations, high gravimetric heat of combustion, and the anticipated synergistic effects from boron and aluminum. Nevertheless, its practical implementation is impeded by intrinsically low energy-release rates and pronounced agglomeration. In this study, two-dimensional graphene fluoride (GF), three-dimensional polytetrafluoroethylene (PTFE), and two-dimensional graphene oxide (GO) were strategically incorporated to construct composite fuel systems capable of fully exploiting the energetic potential of AlB2. Laser-ignition experiments demonstrated that GF, GO, and PTFE all generate abundant gaseous products while markedly intensifying the combustion of AlB2, while GF exhibits better enhancing effects. Thermal analyses reveal that fluorinated additives markedly enhance the thermal oxidation characteristics of AlB2, effecting a pronounced reduction in its initial decomposition temperature. The difference in the combustion mechanism of AlB2 with GF and GO lies in the fluorine, although they both open alternative reaction pathways, GF exhibits more notable capacity to suppress agglomeration of condensed combustion products. The formulation developed and mechanisms revealed by this work could potentially advance the applications of boron-based fuels in ramjets and scramjets.
KW - Aluminum diboride
KW - Combustion mechanism
KW - Functionalized graphene
KW - Laser ignition
KW - Solid propulsion
UR - https://www.scopus.com/pages/publications/105025697869
U2 - 10.1007/s42423-025-00201-6
DO - 10.1007/s42423-025-00201-6
M3 - 文章
AN - SCOPUS:105025697869
SN - 3059-2968
VL - 9
SP - 107
EP - 121
JO - Advances in Astronautics
JF - Advances in Astronautics
IS - 1
ER -