- JP-7
JP-7 (Jet Propellant 7, MIL-T-38219) is a
jet fuel developed by theU.S. Air Force for use insupersonic aircraft because of its highflashpoint and thermal stability. It is the fuel used in thePratt & Whitney J58 engines, used in the LockheedSR-71 Blackbird . The air friction of Mach 3+ cruising flight generates very high skin temperatures, therefore this special fuel was needed. The story told byBen Rich in his book "Skunk Works " is that a lit match can be dropped in a bucket of JP-7 and the fuel will not ignite and match will be extinguished (although this is common in any low-volatility fuel includingkerosene and diesel).JP-7 is a mixture composed primarily of
hydrocarbon s, includingalkane s,cycloalkane s, alkylbenzenes,indane s/tetralin s, andnaphthalene s, with addition offluorocarbon s to increase itslubricant properties, an oxidizing agent to make it burn better, and acaesium containing compound known as A-50, which aided in disguising the radar signature of the exhaust plume.JP-7 is unusual in that it is not a distillate fuel but is created from special blending stocks in order to have very low (<3%) concentration of highly volatile components like
benzene ortoluene , and almost no sulfur, oxygen, and nitrogen impurities. It is specified by MIL-DTL-38219. It has low vapor pressure and high thermal oxidation stability. It has to operate within a wide range of temperatures, from near freezing of high altitudes to high temperature of airframe and engine parts being cooled. Its volatility must be low to make it flash-resistant even in these high temperatures.The very low volatility and relative unwillingness of JP-7 to be ignited required
triethylborane (TEB) to be injected into the engine in order to light it up, and to light up theafterburner in flight.Properties
* Melting Point −30 °C
* Boiling Point (1 atm) 282–288 °C
* Density (at 15 °C) 779–806 kg/m³
* Vapor Pressure (at 300 °F (149 °C)) 155 mmHg (20.7 kPa)
* Flashpoint 60 °C
* Net heat of combustion min. 43.5 MJ/kgFrom the SR-71 Flight Manual:
"The operating envelope of the JT11D-20 engine requires special fuel. The fuel is not only the source of energy but is also used in the engine
hydraulic system. During high Mach flight, the fuel is also aheat sink for the various aircraft and engine accessories which would otherwise overheat at the high temperatures encountered. This requires a fuel having high thermal stability so that it will not break down and deposit coke and varnishes in the fuel system passages. A highluminometer number (brightness of flame index) is required to minimize transfer of heat to the burner parts. Other items are also significant, such as the amount ofsulfur impurities tolerated. Advanced fuels, JP-7 (PWA 535) and PWA 523E, were developed to meet the above requirements."ee also
*
JP-1
*JP-4
*JP-5
*JP-6
*JP-7
*JP-8
*JPTS
*Jet fuel
*Aviation fuel External References
* [http://assist.daps.dla.mil/quicksearch/basic_profile.cfm?ident_number=21921 MIL-T-38219D Military Specification, Turbine Fuel, Low Volatility, JP-7]
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