An arming assembly for a personal self-defense device includes a substantially closed-ended cylindrical member having a first end and a second end, the cylindrical member having an interior chamber. At least one opening being formed within the first end for the inserting and exiting of a porcupine quill. A translatable piston includes a spring and a disc being disposed within the interior chamber. At least one arm being attached to the spring in order to compress and release the spring and translate the disc toward the second end. At least one quill is inserted into the opening formed within the first end and sits in an associated indentation formed within the disc. Once the arm is released, the quill is projected forward and exits through the opening formed within the first end, which is aimed at a would-be attacker. The arming assembly may be double-acting by having conjoined opposed similar components.

The present disclosure relates to a launch system, a launch vehicle for use with the launch system, and methods of launching a payload utilizing the launch vehicle and/or the launch system. The disclosure can provide for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location. The launch vehicle can comprise a payload, a propellant tank, an electrical heater wherein propellant, such as a light gas (e.g., hydrogen) is electrically heated to significantly high temperatures, and an exhaust nozzle from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec. The launch vehicle can be utilized with the launch system, which can further comprise a launch tube formed of at least one tube, which can be electrically conductive and which can be combined with at least one insulator tube. An electrical energy source, such as a battery bank and associated inductor, can be provided.

The object of this invention is a method to shoot an object from a flying apparatus. Into an flying apparatus, into certain part of it, like a container that consists at least of a bottom and a shell a spring will be placed, like a push spring that has been loaded in a tense state and that is locked in this position using a fixing organ and further there will be put as an extension of the spring an object to be shot out from the flying apparatus. The fixing organ is thread, metal cord, bar, strip, rope, line, or some combination of these and tension strength (T) is greater than the tension load of the push force (F) to the mentioned fixing organ. the tension strength (T) of the fixing organ is weakened to be less than the mentioned tension load by heating, burning, or melting the mentioned fixing organ by electric energy when the fixing organ breaks, the spring expands into the direction of the object and the push force (F) pushes the object out of the container and off the flying apparatus. The apparatus that is used in the present method is also an object of the invention.

A robotic vehicle is provided with vertical ball cannon and a ball deflector. The ball deflector is mounted over the vertical ball cannon on a vertical linear slide. The deflector redirects a ball shot from the cannon toward a desired target, such as a cylindrical goal. The vehicle further includes a rotating goal-grabber for anchoring a goal adjacent to the vehicle and underneath the output of the deflector. A pair of counter-rotating helical screws capture a ball from the ground and raise it into the ball cannon. The cannon launches the ball toward the deflector, which redirects the ball's upward vertical motion away from the cannon into a downward vertical motion toward the desired target.

A robotic vehicle is provided with vertical ball cannon and a ball deflector. The ball deflector is mounted over the vertical ball cannon on a vertical linear slide. The deflector redirects a ball shot from the cannon toward a desired target, such as a cylindrical goal. The vehicle further includes a rotating goal-grabber for anchoring a goal adjacent to the vehicle and underneath the output of the deflector. A pair of counter-rotating helical screws capture a ball from the ground and raise it into the ball cannon. The cannon launches the ball toward the deflector, which redirects the ball's upward vertical motion away from the cannon into a downward vertical motion toward the desired target.

A modular disruptor cannon includes three open-ended tubular structures. A first tubular housing defines a first interior region longitudinally aligned with a second interior region. The first tubular housing has external-surface threads at a first end thereof adjacent to the second interior region. A tubular insert is fitted in the second interior region. A second tubular housing defines a cap longitudinally aligned with a barrel. The barrel has an inside diameter equal to the inside diameter of the tubular insert. The cap has internal-surface threads for mating with the external-surface threads of the first tubular housing where the barrel is longitudinally aligned with the tubular insert.

A modular disruptor cannon includes three open-ended tubular structures. A first tubular housing defines a first interior region longitudinally aligned with a second interior region. The first tubular housing has external-surface threads at a first end thereof adjacent to the second interior region. A tubular insert is fitted in the second interior region. A second tubular housing defines a cap longitudinally aligned with a barrel. The barrel has an inside diameter equal to the inside diameter of the tubular insert. The cap has internal-surface threads for mating with the external-surface threads of the first tubular housing where the barrel is longitudinally aligned with the tubular insert.

A cannon includes: a barrel; a breech ring connected to the rear of the barrel; a breechblock connected to be movable with respect to the breech ring between a closed position and an open position; an ignition device mounted to be partially movable with respect to the breechblock and configured to ignite a propelling charge; and a controller configured to transfer an electrical firing signal, wherein the ignition device includes: a firing assembly moving forward and backward as the breechblock moves; a laser diode primer connected to the front of the firing assembly and configured to receive the electrical firing signal to ignite the propelling charge; and a firing pin connected to be movable forward and backward with respect to the firing assembly and configured to transfer the electrical firing signal to the laser diode primer while in contact with a rear end of the laser diode primer.

A cannon includes: a barrel; a breech ring connected to the rear of the barrel; a breechblock connected to be movable with respect to the breech ring between a closed position and an open position; an ignition device mounted to be partially movable with respect to the breechblock and configured to ignite a propelling charge; and a controller configured to transfer an electrical firing signal, wherein the ignition device includes: a firing assembly moving forward and backward as the breechblock moves; a laser diode primer connected to the front of the firing assembly and configured to receive the electrical firing signal to ignite the propelling charge; and a firing pin connected to be movable forward and backward with respect to the firing assembly and configured to transfer the electrical firing signal to the laser diode primer while in contact with a rear end of the laser diode primer.

Disclosed is a cannon including: a barrel having a chamber in which a shell and a propelling charge are mounted; a breech ring connected to the rear of the barrel, and having a shell inlet communicating with the chamber; a recoil buffer disposed on an outer circumferential surface of the barrel, and guiding recoiling and returning motions of the barrel; a breechblock connected to the breech ring, and moving relative to the breech ring between a closed position closing the shell inlet and an open position opening the shell inlet; a laser ignition device including a laser portion disposed in the breechblock and emitting a laser to ignite the propelling charge, and a breech window covering the laser portion and allowing the laser to be transmitted into the chamber; and a breech window cleaning device cleaning the breech window.