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Jet Fuel Thermal Stability Additives - Electrical Conductivity and Interactions with Static Dissipator Additive
Technical Paper
2002-01-1652
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The primary goal of the USAF JP-8+100 thermal stability additive (TSA) program is to increase the heat-sink capacity of JP-8 fuel by 50%. Current engine design is limited by a fuel nozzle temperature of 325°F (163°C); JP-8+100 has been designed to allow a 100°F increase in nozzle temperatures up to 425°F (218°C) without serious fuel degradation leading to excessive deposition. Previous studies have shown that TSA formulations increase the electrical conductivity of base jet fuel. In the present paper, further characterization of this phenomenon is described, as well as interactions of newer TSAs with combinations of SDA and other surface-active species in hydrocarbons, will be discussed.
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Authors
Citation
Taylor, S., Forester, D., and Malik, B., "Jet Fuel Thermal Stability Additives - Electrical Conductivity and Interactions with Static Dissipator Additive," SAE Technical Paper 2002-01-1652, 2002, https://doi.org/10.4271/2002-01-1652.Also In
References
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- Dacre B. Hetherington J.I. Proceedings of the 6 th International Conference on Stability and Handling of Liquid Fuels Vancouver, BC October 13-17 1997 315 332
- Dacre B. Hetherington J.I. Longjohn R. Proceedings of the 7 th International Conference on Stability and Handling of Liquid Fuels Graz, Austria September 24-29 2000 571 589