Low viscosity-high flash point ramjet and turbojet fuels

Fuel and related compositions – Liquid fuels – Aluminum or heavy metal – other than lead – containing

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C10L 116

Patent

active

040280667

ABSTRACT:
A method for propelling a ramjet or turbojet engine wherein a fuel consisg essentially of a mixture of a fraction of petroleum distillate having a boiling point of from 380.degree. F to 415.degree. F and butylbenzene is used.

REFERENCES:
patent: 1879118 (1932-09-01), Davidson
patent: 2211732 (1940-08-01), Sachanen et al.
patent: 2305026 (1942-12-01), Munday
patent: 2749225 (1956-06-01), Barnum et al.
patent: 3817721 (1974-06-01), Perilstein

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