Abstract: The invention describes and claims an apparatus and method of missile interception. The missile interceptor comprises a net body with a plurality of sections and at least one missile trajectory effector. In the preferred variant, the missile trajectory effector is embodied as an exploding ring. A missile, passing through the net body, picks up a ring, which explodes once the missile passes a sufficient distance away from the missile interceptor. Preferred embodiments of the missile interceptor further comprise one or more vertically-positioned poles. Claimed method involves the use of such interceptor and positioning the interceptor on the likely trajectory of incoming missiles.

Abstract: An air transport vehicle of the present invention comprises a tubular body, said body comprising an upper half and a lower half. The upper half is positioned above the lower half and connected thereto. A central bore is formed between the upper half and the lower half. The bore extends longitudinally from the nose end of the vehicle to the tail end of the vehicle. The vehicle also comprises at least one propulsion device, preferably positioned inside the bore. The vehicle further comprises at least one bulkhead. The bulkhead connects the upper half to the lower half, and extending longitudinally inside the bore, thus dividing the bore into parallel subsections. In preferred embodiments, the upper half and the lower half comprise cavities, used among other things, for cargo and passenger transport.

Abstract: The ship body of the present invention comprises at least two levels. One is an upper level that comprises a floatable body. The other is a lower level. The lower level is intended to be submerged under water in normal use. The lower level comprises at least two parallel, essentially vertical walls, a floor, and a ceiling connecting the at least two parallel essentially vertical walls. The front end and a rear end of the lower level are open to allow water to enter through the front end and exit through the rear end of the lower level.

Abstract: The method of interrupting a tornado comprises the step of locating an area of ongoing tornadic activity. Ultra-cold substance is then released at low altitudes in the area of ongoing tornadic activity. In preferred embodiments, the ultra-cold substance is delivered to the area of ongoing tornadic activity by an airplane. The ultra-cold substance is preferably liquid nitrogen.

Abstract: The invention describes and claims an apparatus and method of missile interception. The missile interceptor comprises a net body with a plurality of sections and at least one missile trajectory effector. In the preferred variant, the missile trajectory effector is embodied as an exploding ring. A missile, passing through the net body, picks up a ring, which explodes once the missile passes a sufficient distance away from the missile interceptor. Preferred embodiments of the missile interceptor further comprise one or more vertically-positioned poles. Claimed method involves the use of such interceptor and positioning the interceptor on the likely trajectory of incoming missiles.

Abstract: The invention describes and claims a method of interrupting a tornado. As the first step, an area of ongoing tornadic activity is located. Ultra-cold substance is then released at low altitudes in the area of ongoing tornadic activity. In preferred embodiments, the ultra-cold substance is delivered to the area of ongoing tornadic activity by an airplane. The ultra-cold substance is preferably liquid nitrogen. In alternative embodiments, detonation of explosives may be used in leu of or in conjunction with the use of the ultra-cold substance to interrupt a tornado.

Abstract: The ship body of the present invention comprises at least two levels. One is an upper level that comprises a floatable body. The other is a lower level. The lower level is intended to be submerged under water in normal use. The lower level comprises at least two parallel, essentially vertical walls, a floor, and a ceiling connecting the at least two parallel essentially vertical walls. The front end and a rear end of the lower level are open to allow water to enter through the front end and exit through the rear end of the lower level.

Abstract: A versatile watercraft of the present invention comprises a base wing, a C-wing, and preferably a plurality of vertical stabilization knives. The base wing extends horizontally from the right side of the watercraft to the left side of the watercraft, and longitudinally, for at least a third of the length of the watercraft. The C-wing, extends above the base wing. The C-wing is comprised of at least two essentially vertical walls and an essentially horizontal top. The watercraft also comprises at least one propulsion device. In the preferred embodiments, a plurality of vertical stabilization knives extends vertically below the base wing and extends longitudinally for at least a third of the length of the watercraft.

Abstract: An air transport vehicle of the present invention comprises a tubular body, said body comprising an upper half and a lower half. The upper half is positioned above the lower half and connected thereto. A central bore is formed between the upper half and the lower half. The bore extends longitudinally from the nose end of the vehicle to the tail end of the vehicle. The vehicle also comprises at least one propulsion device, preferably positioned inside the bore. The vehicle further comprises at least one bulkhead. The bulkhead connects the upper half to the lower half, and extending longitudinally inside the bore, thus dividing the bore into parallel subsections. In preferred embodiments, the upper half and the lower half comprise cavities, used among other things, for cargo and passenger transport.