A major increase in terminal explosive energy of a missile by reacting bulk aluminum, titanium, magnesium, steel, and/or organic matrix composite missile structure with oxygen enriched air which is collected as the missile flies to its target. Oxygen rich air is produced from a small amount of engine bleed or atmospheric air processed through a molecular sieve on board oxygen generating system (OBOG), and stored under pressure in the missile fuel tanks as they are emptied during flight. Explosive reaction of the oxygen with missile structure is achieved with a flexible linear shaped charge (FLSC) attached to tank wall structure. Initiation of an explosive reaction between the bulk aluminum and oxygen can be achieved by a conventional shape charge or the like.
A neutralization device for a payload carried by a vector, such as a rocket. This device incorporates at least one explosively-formed charge, where such charge is made integral with the vector by a positioning device ensuring the orientation of its direction of action towards the payload.
A weapon transport device transports along a path toward a target in hostile territory, (1) a target-intended weapon and (2) biological, chemical and/or radioactive agents for attacking the occupants of such territory should they execute countermeasures against the weapon transport device. Separation of the biological, chemical and/or radioactive agents is initiated or, where appropriate, inhibited, by signals from either the guidance system of the transport device or from on-board Global Positioning System (GPS) receivers when the transport device strays by more than a predetermined distance from the path, the sensor is blinded, or the transport device passes beyond a predetermined point while en route to the target.
