Abstract
Aluminum-water (Al-H2O) propellant is a promising class of environmentally friendly propellants with the potential to reduce harmful emissions associated with conventional solid propellants, thereby mitigating environmental pollution. However, current formulations of Al-H2O propellants generate substantial solid residues upon combustion, which can reduce specific impulse and pose a risk of nozzle blockage. To enhance the combustion and injection behavior of Al-H2O propellants, this work presents a novel approach that modifies aluminum powder with bismuth oxide (Bi2O3), harnessing their intrinsic chemical interaction. Thermogravimetric analysis and laser ignition experiments demonstrate that the incorporation of Bi2O3 improves the injection efficiency of Al-H2O gelled propellants while reducing the formation of solid combustion residues. This enhancement is attributed to the reaction between Bi2O3 and aluminum, which increases the production of gaseous combustion products. In addition to its catalytic effect, Bi2O3 significantly mitigates aluminum agglomeration during combustion, contributing to improved combustion efficiency in Al-H2O gelled propellants. The incorporation of 10 wt% Bi2O3 notably boosted injection efficiency from 27.95 % to 54.76 %, while combustion efficiency increased from 80.15 % to 89.56 %. Hot firing of rocket motor tests further demonstrated that the incorporation of 10 wt% Bi2O3 led to an increase in specific impulse from 1270 N·s/kg to 2001 N·s/kg, highlighting the significant enhancement in propulsion performance. The findings of this study provide valuable insights into the performance optimization of Al-H2O gelled propellants, offering a new perspective on their formulation and application.
Original language | English |
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Article number | 135670 |
Journal | Fuel |
Volume | 399 |
DOIs | |
State | Published - 1 Nov 2025 |
Keywords
- Agglomeration
- Aluminum-water propellants
- Bismuth oxide
- Combustion
- Injection
- Rocket motor