TY - JOUR
T1 - Effects of aluminum on combustion characteristic of HTPE propellants
AU - Liang, Bei
AU - Zhang, Ning
AU - Liu, Changyi
AU - Xia, Min
AU - Zhang, Weihai
AU - Gao, Xifei
N1 - Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
PY - 2023
Y1 - 2023
N2 - The surface morphology of four kinds of aluminum powders with different particle sizes was observed by scanning electron microscope (SEM), and the effects of four different particle sizes of aluminum powder on the combustion performance of HTPE propellant were studied by means of underwater acoustic emission method, differential sanning calorimetry and high-speed photography. The results show that the smaller the particle diameters of aluminum powder, the higher the burning rate pressure index of HTPE propellant, and its pressure index will increase from 0.26 to 0.48 in the pressure range of 5-11MPa. And as the particle size of aluminum powder decreases, the combustion activation energy shows a decreasing trend. When the pressure increases from 2MPa to 4MPa, as the particle size of the aluminum powder decreases, its specific surface area increases, the reaction activity becomes higher, and the aluminum powder combustion performance becomes more intense and sufficient, the maximum combustion flame temperature of the propellant increased from 2375°C∼2403°C to 2425 °C ∼2482 °C, respectively, and the overall flame temperature fluctuation range was relatively small.
AB - The surface morphology of four kinds of aluminum powders with different particle sizes was observed by scanning electron microscope (SEM), and the effects of four different particle sizes of aluminum powder on the combustion performance of HTPE propellant were studied by means of underwater acoustic emission method, differential sanning calorimetry and high-speed photography. The results show that the smaller the particle diameters of aluminum powder, the higher the burning rate pressure index of HTPE propellant, and its pressure index will increase from 0.26 to 0.48 in the pressure range of 5-11MPa. And as the particle size of aluminum powder decreases, the combustion activation energy shows a decreasing trend. When the pressure increases from 2MPa to 4MPa, as the particle size of the aluminum powder decreases, its specific surface area increases, the reaction activity becomes higher, and the aluminum powder combustion performance becomes more intense and sufficient, the maximum combustion flame temperature of the propellant increased from 2375°C∼2403°C to 2425 °C ∼2482 °C, respectively, and the overall flame temperature fluctuation range was relatively small.
KW - Aluminum
KW - Combustion behavior
KW - HTPE
KW - Propellant
UR - http://www.scopus.com/inward/record.url?scp=85167424940&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/2478/3/032033
DO - 10.1088/1742-6596/2478/3/032033
M3 - Conference article
AN - SCOPUS:85167424940
SN - 1742-6588
VL - 2478
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
IS - 3
M1 - 032033
T2 - 3rd International Conference on Defence Technology, ICDT 2022
Y2 - 22 August 2022 through 26 August 2022
ER -