Method of confinement of propellants for ignition

Ordnance – Pneumatic

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102202, F41A 104

Patent

active

053599195

ABSTRACT:
A method for confinement of a gun propellant during the initial stage of ignition provides the ignition by electrical, pyrotechnic, or laser irradiation means. A liquid and or a solid propellant is placed in a substantially closed chamber. A portion of the propellant in a conduit of the chamber exits from the chamber and is cooled in the exit conduit by a thermoelectric or cryogenic means to a sufficiently low temperature for producing a viscous, glassy, or substantially solidified condition to enhance the propellant containment. An ignition stimulus is then applied. A closure means in the exit conduit selectively varies the amount of flow whereby a relatively high temperature and pressure are reached from the chemical energy release of the propellant. Venting of the formed combustive products is provided through the exit conduit whereby sufficient thermal energy is generated to sustain combustion and to ignite the next stage.

REFERENCES:
patent: 3528372 (1970-09-01), Lewis et al.
patent: 3759183 (1973-09-01), Apstein
Twenty-First Symposium (International) on Combustion/ The Combustion Instte Plasma Propellant Jet Ignition, by F. B. Carleton, et al, 1986, pp. 1885-1890.
Memorandum Report BRL-MR-3748, Electrical Ignition of LGP 1846 in a Two Stage Igniter, by James DeSpirito, et al, Apr. 1989.

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