A munitions dispenser employs a plurality of launch tubes mounted in an array as a segmented dispenser assembly. Each tube in the array is configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture. A frame, mountable to an air vehicle, carries the array of launch tubes. A skin covers the array of launch tubes with the skin and frame with the array configured for nested engagement of multiple segmented assemblies.

A munitions dispenser employs a plurality of launch tubes mounted in an array as a segmented dispenser assembly. Each tube in the array is configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture. A frame, mountable to an air vehicle, carries the array of launch tubes. A skin covers the array of launch tubes with the skin and frame with the array configured for nested engagement of multiple segmented assemblies.

A low-cost, reliable and easy to use kit for neutralizing surface exposed landmine and unexploded ordnance for humanitarian demining is based on a liquid fuel and a solid/soluble fuel. Both fuels are premeasured in separate, sealed containers. The addition of a small quantity of solid/soluble fuel into the liquid creates an explosive. The resulting mixture is capable of detonating with a standard No. 8 blasting cap. The solid/soluble fuel can be in the form of a powder, tablet, or its saturated solution in water. The solid/soluble fuel is hexamethylenetetramine. The liquid fuel, nitromethane, is provided in premeasured quantities. User is provided instructions for choosing the appropriate quantity of liquid fuel, the corresponding solid/soluble fuel required, the method of mixing, placement and detonation of the kits. Also disclosed is a simple wooden stand to hold the bottle of explosive in place. A special fuel, liquid 2-ethylhexylnitrate, is provided to desensitize the mixed and sensitized explosive.

A method for focusing a beam of a high energy radiation source on a reference point on the surface of a flying object, comprising: recording a number of consecutive two-dimensional images of the flying object determining the trajectory of the flight path simultaneously determining the line of sight angle between the image acquisition device and the position of the flying object calculating a three-dimensional model of the flying object displaying the currently acquired two-dimensional image marking the reference point on the displayed two-dimensional image of the flying object; calculating the three-dimensional reference point on the surface of the flying object focusing the beam of the high energy radiation source on the three-dimensional reference point.

A weapon interface system, and methods of operating the same. The weapon interface system is coupled to an electrical interconnection system of a delivery platform and a weapon system coupled to a rack system. The weapon interface system includes a translation interface configured to provide an interface between the electrical interconnection system and an inductive power and data circuit. The weapon interface system also includes a weapon coupler, coupled to the translation interface, configured to provide an inductive coupling to the weapon system to provide mission information thereto.

A munitions dispenser employs a plurality of launch tubes mounted in an array as a segmented dispenser assembly. Each tube in the array is configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture. A frame, mountable to an air vehicle, carries the array of launch tubes. A skin covers the array of launch tubes with the skin and frame with the array configured for nested engagement of multiple segmented assemblies.

A munitions dispenser employs a plurality of launch tubes mounted in an array as a segmented dispenser assembly. Each tube in the array is configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture. A frame, mountable to an air vehicle, carries the array of launch tubes. A skin covers the array of launch tubes with the skin and frame with the array configured for nested engagement of multiple segmented assemblies.

A weapon interface system, and methods of operating the same. The weapon interface system is coupled to an electrical interconnection system of a delivery platform and a weapon system coupled to a rack system. The weapon interface system includes a translation interface configured to provide an interface between the electrical interconnection system and an inductive power and data circuit. The weapon interface system also includes a weapon coupler, coupled to the translation interface, configured to provide an inductive coupling to the weapon system to provide mission information thereto.

A weapon interface system, and methods of operating the same. The weapon interface system is coupled to an electrical interconnection system of a delivery platform and a weapon system coupled to a rack system. The weapon interface system includes a translation interface configured to provide an interface between the electrical interconnection system and an inductive power and data circuit. The weapon interface system also includes a weapon coupler, coupled to the translation interface, configured to provide an inductive coupling to the weapon system to provide mission information thereto.