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http://dx.doi.org/10.6108/KSPE.2014.18.5.095

Improvement of Heat of Reaction of Jet Fuel Using Pore Structure Controlled Zeolite Catalyst  

Hyeon, Dong Hun (Department of Chemical & Biological Engineering, Graduate School, Korea University)
Kim, Joongyeon (Department of Chemical & Biological Engineering, Graduate School, Korea University)
Chun, Byung-Hee (Department of Chemical & Biological Engineering, Graduate School, Korea University)
Kim, Sung Hyun (Department of Chemical & Biological Engineering, Korea University)
Jeong, Byung-Hun (Advanced Propulsion Technology Center, Agency for Defense Development)
Han, Jeong Sik (Advanced Propulsion Technology Center, Agency for Defense Development)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.18, no.5, 2014 , pp. 95-100 More about this Journal
Abstract
In hypersonic aircraft, increase of aerodynamic heat and engine heat leads heat loads in airframe. It could lead structural change of aircraft's component and malfunctioning. Endothermic fuels are liquid hydrocarbon fuels which are able to absorb the heat load by undergoing endothermic reactions. In this study, exo-tetrahydrodicyclopentadiene was selected as a model endothermic fuel and experiments on endothermic properties were investigated with pore structure controlled zeolite catalyst using metal deposition. We secured the catalyst that had better endothermic performance than commercial catalyst. The object of this study is inspect catalyst properties which have effect on heat absorption improvement. Synthetic catalyst could be applied to system that use exo-THDCP as endothermic fuel instead of other commercial catalyst.
Keywords
Hypersonic Aircraft; Endothermic Fuel; Zeolite; exo-THDCP(exo-tetrahydrodicyclopentadiene;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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