Thermal Decomposition Kinetics of the Thermally Stable Jet Fuels JP-7, JP-TS and JP-900

Author:

Gough Raina V.1,Widegren Jason A.1,Bruno Thomas J.1

Affiliation:

1. NIST Boulder, Boulder, Colorado 80305, United States

Publisher

American Chemical Society (ACS)

Subject

Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Reference52 articles.

1. Detail Specification: Turbine Fuel, Low Volatility, JP-7;MIL-DTL-38219D;Wright-Patterson AFB:Wright-Patterson AFB, OH, 1998.

2. A Comparison of the Hypersonic Vehicle Fuel JP-7 to the Rocket Propellants RP-1 and RP-2 with the Advanced Distillation Curve Method

3. Detail Specification: Turbine Fuel, Aviation, Thermally Stable;MIL-DTL-25524E;Wright-Patterson AFB:Wright-Patterson AFB, OH, 1997.

4. Detail Specification: Propellant Rocket Grade Kerosene;MIL-DTL-25576D;Wright-Patterson AFB:Wright-Patterson AFB, OH, 2005.

5. Billingsley, M.; Edwards, T.; Shafer, L. M.; Bruno, T. J.Extent and Impacts of Hydrocarbon Fuel Compositional Variability for Aerospace Propulsion Systems. In46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, TN, July 25–28, 2010.

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