JP-10 (fuel)

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JP-10 fuel (Jet Propellant 10) is a jet fuel, specified and used mainly as fuel in missiles. Being designed for military purposes, it is not a kerosene based fuel.

Contents

Developed to be a gas turbine fuel for cruise missiles, [1] it contains mainly exo-tetrahydrodicyclopentadiene (a synthetic fuel), and adamantane.[ citation needed ] However, it is usually classed as a single component fuel, as well as a hydrocarbon. [2] It is produced by catalytic hydrogenation of dicyclopentadiene and then isomerization.

It superseded JP-9, which is a mixture of norbornadiene-based RJ-5 fuel, tetrahydrodicyclopentadiene and methylcyclohexane, because of a lower temperature service limit and about four times lower price. [3] Since the lack of volatile methylcyclohexane makes its ignition difficult, a separate priming fluid PF-1 with about 10-12% of this additive is required for the engine start-up. [3] Its main use is in the Tomahawk missiles. [4]

The Russian equivalent is called detsilin .

Chemical properties of JP-10 fuel

Uses

JP-10 absorbs heat energy, so is endothermic with a relatively high density of 940 kg/m3. It has a low freezing point of less than −110 °C (−166 °F) and the flash point is 130 °F (54 °C). The high energy density of 39.6 MJ/L makes it ideal for military aerospace applications - its primary use. The ignition and burn chemistry has been extensively studied. [8] [9] [10] The exo isomer also has a low freezing point. [11] [12] Its other properties have also been studied extensively. [13] [14] [15] [16] [17]

Even though its uses are mainly for the military, the relatively high cost has meant research has been undertaken to find lower costs routes including the use of cellulosic materials. [18]

Further research

Current and past areas of research focus on:

Related Research Articles

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3
NO
2
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Further reading