Combustion Characterization for Paraffin-Based Gas Generator with End-Burning

A paraffin-based hybrid gas generator (HGG) with end-burning offers a cost-effective and flow-adjustable gas supply solution for trans-medium systems. To deliver high-quality fuel-rich gas, the combustion dynamics were analyzed theoretically. Using a laboratory-scale HGG with oxygen flow rates of [Formula: see text], firing tests were then conducted to evaluate the combustion characteristics, including ignition, pressure oscillation, regression rate, oxidizer-to-fuel ratio, and combustion temperature. The performance of solid fuels, including polyethylene, pure paraffin, aluminum-loaded paraffin, and paraffin-based fuels, was compared, and the effect of grain structures, including conventional and nested spiral structures, was investigated. The polyethylene fuel grain was tested and served as the baseline. The combustion process with rapid ignition was stable with no observed oscillations. Pure paraffin fuel exhibited superior regression rates that were linearly dependent on oxidizer flux, proving that it is well-suited for HGG. Binders and aluminum additives reduced regression rates by up to 63% and elevated combustion temperatures. Excess aluminum further suppressed regression rates and raised oxidizer-to-fuel ratios. Furthermore, the nested spiral structure enhanced regression rates by 8.6% while preserving the end-burning grain structure. Ultimately, the successful ignition of the water ramjet engine using aluminum-loaded paraffin fuel grains validates the application potential of the HGG.

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Publication Details

Journal
Journal of Spacecraft and Rockets
Published
2025-12-21
DOI
https://doi.org/10.2514/1.a36453
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
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article

Combustion Characterization for Paraffin-Based Gas Generator with End-Burning

Journal of Spacecraft and Rockets
Rocket and propulsion systems research
article

Combustion Characterization for Paraffin-Based Gas Generator with End-Burning

article en

Abstract

A paraffin-based hybrid gas generator (HGG) with end-burning offers a cost-effective and flow-adjustable gas supply solution for trans-medium systems. To deliver high-quality fuel-rich gas, the combustion dynamics were analyzed theoretically. Using a laboratory-scale HGG with oxygen flow rates of [Formula: see text], firing tests were then conducted to evaluate the combustion characteristics, including ignition, pressure oscillation, regression rate, oxidizer-to-fuel ratio, and combustion temperature. The performance of solid fuels, including polyethylene, pure paraffin, aluminum-loaded paraffin, and paraffin-based fuels, was compared, and the effect of grain structures, including conventional and nested spiral structures, was investigated. The polyethylene fuel grain was tested and served as the baseline. The combustion process with rapid ignition was stable with no observed oscillations. Pure paraffin fuel exhibited superior regression rates that were linearly dependent on oxidizer flux, proving that it is well-suited for HGG. Binders and aluminum additives reduced regression rates by up to 63% and elevated combustion temperatures. Excess aluminum further suppressed regression rates and raised oxidizer-to-fuel ratios. Furthermore, the nested spiral structure enhanced regression rates by 8.6% while preserving the end-burning grain structure. Ultimately, the successful ignition of the water ramjet engine using aluminum-loaded paraffin fuel grains validates the application potential of the HGG.

Journal of Spacecraft and Rockets
China Academy of Space Technology (CN), Chinese Academy of Sciences (CN), Digital Solid State Propulsion (United States) (US)
Openalex Percentile: Top 47%
Rocket and propulsion systems research
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