Thermal Stability and Heat Transfer Characteristics of RP-2
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Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Liquid Fuels and Propellants for Aerospace Propulsion: 1903-2003
2. Irvine, S.A.,Schoettmer, A.K., Bates, R.W., andMeyer,M.L. "HistoryofSulfur Content Effects on the Thermal Stability of RP-1 Under Heated Conditions," (AIAA) 2004-3879 at 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Fort Lauderdale,FL, 2004.
3. Stiegemeier,B., Meyer, M.L., and Taghavi, R. "AThermalStabilityand Heat Transfer Investigation ofFive Hydrocarbon Fuels:JP-7, JP-8, JP-8+100,JP-10, and RP-1,"(AIAA) 2002-3873at 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis,IN, 2002.
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