U.S. Patent Specifications

Abstract

In combination, an aerial missile having a body in the form of an elongated tubular duct, a diffuser in said duct, a pressurized fuel source having a fuel chamber in said body, nozzle means connected with said fuel chamber and communicating with said duct, a venturi for said nozzle means and igniter means in said duct, said igniter means including at least an upstream flameholder and a downstream flameholder, with a source of ignition in said upstream flameholder, said nozzle means being spaced upstream from said igniter means and arranged to inject fuel into an airstream passing through said venturi at the throat thereof in a direction contra to the flow of said airstream therethrough.

Citation

(1959), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 31 No. 1, pp. 30-30. https://doi.org/10.1108/eb033075