EA202000019A1 - AIRCRAFT FOR DESTRUCTION OF ASTEROIDS USING ATMOSPHERIC ELECTRICITY (BLESKIN-CHURAKOVA GRAVITALET "BECH" 2) - Google Patents

Abstract

An aircraft for the destruction of asteroids by laser radiation using atmospheric electricity differs in that it consists of a ball made of a durable elastic, heat-resistant material with a metallized coating on the outside, filled with air, having an air heater inside, outside a compressor for supplying air to the ball and a valve air discharge from the ball, coupled to the fuselage, covered with a material with increased electrical conductivity, in the form of a cone truncated from above with a base in the form of a metal disc, inside the fuselage there is a hemispherical depression made of metal, a wing made of metal in the form of a disc, including four fenders located in parallel the base under the fuselage and attached to it with four metal supports, a rudder located vertically in the center between the base of the fuselage and the wing, four control rods of the wing liner, four rocket motors located crosswise under the lower surface of the wing nozzles ami outward from the center, and four support legs, control panel in the fuselage cockpit; an electrical station, consisting of a receiving unit in the form of a fuselage and from it, a needle covered with a dielectric descends from its surface, the end of which is connected to the upper disk of the capacitor, which is enclosed in a dielectric chamber, from the base there is a needle covered with a dielectric, at the top of which is fixed the lower disk of the capacitor, an air network is connected to the upper needle, on the upper branch of which there is a spark gap, the second electrode of which is connected to an inductance coil, which is connected to the lower needle, the second self-inductance coil is connected to a rectifier connected to a large-capacity capacitor connected to a battery ( charged initially from the mains, then from atmospheric electricity), the capacitor is enclosed in a dielectric chamber and has a spark gap, to protect the battery from overcharging on the upper and lower needles, a double switch is introduced, the battery charge indicator is connected to it (the battery), for remote the power plant is controlled by a remote control unit connected to a double switch and a battery charge indicator, for example, a voltmeter; protection of the power plant, which is located in the aircraft, from external influences, operational safety is carried out, completely insulating, a metal casing covered with a dielectric, the fuselage is covered with a material with increased electrical conductivity to enhance the accumulation of atmospheric electricity, the lower needle, insulated with a dielectric from the base of the fuselage, exits through the lower surface of the fuselage to the atmosphere through a switch, connected to a folding antenna covered with a dielectric, the peripheral end of which is exposed, the power station located inside the fuselage for protection from external influences and influences is completely isolated by a metal casing covered with a dielectric, a voltage converter connected to a battery and laser device. The aircraft is able to overcome gravity and go out into the stratosphere and space, carry out a controlled flight in the Earth's orbit and return to the launch site in a manned mode.