Exquadrum, Inc.

Other

United States of America As Represented by the Secretary of the Air Force

Robert L Geisler

Kevin E Mahaffy

Francisco Q Roberto

Arnold M Crelier

A kinetic fireball incendiary munition is provided having an outer shell or bomb casing, one or more incendiary sub munitions therein, and an igniter therefore. Each of the submunitions includes an incendiary portion, at least one rocket motor that propels the submunition inside of a target volume, and an oxidizer for the incendiary portion and rocket motor. The submunitions liberate sufficient heat to produce elevated temperatures inside of a target structure to thermalize the contents thereof without creating a substantial overpressure or explosive effect.

Kinetic fireball incendiary munition

A kinetic fireball incendiary munition is provided having an outer shell or bomb casing, one or more incendiary submunitions therein, and an igniter therefore. Each of the submunitions includes an incendiary portion, at least one rocket motor that propels the submunition inside of a target volume, and an oxidizer for the incendiary portion and rocket motor. The submunitions liberate sufficient heat to produce elevated temperatures inside of a target structure to thermalize the contents thereof without creating a substantial overpressure or explosive effect. The incendiary portion includes a solid propellant and, optionally, one or more energetic materials selected from the group consisting of phosphorous, boron, magnesium, aluminum, Fluorinert&#x2122;-aluminum and BKNO. The incendiary submunition may be in the shape of a ball or a circular disk with a rocket motor therein. The circular disk-shaped incendiary munition is provided with an outer layer of an insulation which is bonded to the propellant/incendiary material. A portion of the insulation on the top and bottom of the disk is weakened so as to break away when the top and bottom surfaces are ignited. In place of the rocket motor, the submunition may incorporate one or more barrels embedded in the incendiary material with a powder charge and projectile in each barrel. Ignition of the incendiary material results in detonation of the powder charge which propels projectiles radially outwardly and upwardly causing damage to containers of chemical/biological materials.

A solid propellant thrust control system, method, and apparatus for controlling combustion of solid propellants in an opposing grains solid propellant rocket engine (OGRE) is provided. In particular, an opposing grains rocket engine and propulsion system is provided, in which actuator means connected are connected to solid propellant grains disposed in the pressure vessel of the engine. The actuator means are operable to selectively move the solid propellant grains together or apart relative to one another, such that the burning ends of the solid propellant grains decrease or increase relative to one another. This action controls the rate of combustion of the solid propellant grains by varying spacing distance between the burning ends of the solid propellant grains, and enables extinguishment and reignition of the OGRE. Further, a method is providing for controlling the burn rate of solid propellant grains undergoing combustion in an opposing grains rocket engine.

Propulsion system, opposing grains rocket engine, and method for controlling the burn rate of solid propellant grains

A kinetic fireball incendiary munition is provided having an outer shell or bomb casing, one or more incendiary submunitions therein, and an igniter therefore. Each of the submunitions includes an incendiary portion and at least one rocket motor that propels the submunition inside of a target volume. The submunitions liberate sufficient heat to produce elevated temperatures inside of a target structure, without creating a substantial overpressure or explosive effect. The incendiary portion includes a solid propellant and, optionally, one or more energetic materials selected from the group consisting of phosphorous, boron, magnesium, aluminum, Fluorinert&#x2122;-aluminum and BKNO. The incendiary submunition may be in the shape of a ball or a circular disk with a rocket motor therein.

A method for improving the ballistic properties of aluminum powder based rocket propellants by treating the aluminum powder with hydrogen fluoride gas prior to its incorporation into a propellant formulation.

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Tehachapi, CA, United States of America

Robert L Geisler