Low viscosity air breathing missile fuel

Explosive and thermic compositions or charges – Miscellaneous compositions

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Details

1491096, 585 14, 585 22, 585253, 585362, D03D 2300

Patent

active

044274670

ABSTRACT:
An improved ramjet fuel consisting of hydrogenated hydrocarbons uses a mium weight percentage of 50% tetrahydromethylcyclopentadiene dimer (TH-dimer) with about 50% by wt. exo-tetrahydrodicyclopentadiene (Exo-THDC). The mixture exceeds U.S. Navy flash point requirements of 60.degree. C. while yielding a lower viscosity than TH-dimer alone. Volumetric heating properties of the mixture make it an excellent ramjet fuel.

REFERENCES:
patent: 3004384 (1961-10-01), Saunders
patent: 4277636 (1981-07-01), Norton et al.

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