Method to control hurricanes by short circuiting the electrical charges with salt water streams
US-2024226946-A1 · Jul 11, 2024 · US
US11570954B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11570954-B2 |
| Application number | US-202017075861-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 21, 2020 |
| Priority date | Aug 28, 2020 |
| Publication date | Feb 7, 2023 |
| Grant date | Feb 7, 2023 |
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Provided is a rocket for artificial rainfall using an ejection hygroscopic flare, the rocket including: a rocket body configured to descend with a parachute after flight by thrust, and having a hygroscopic flare discharge outlet; a communication module installed in the rocket body, and configured to transmit and receive a launch command and an ejection command with a ground station; an ejection hygroscopic flare installed in the rocket body and filled with cloud seeds and a burning material therein; and a hygroscopic flare ejection device configured to separate and eject the ejection hygroscopic flare from an inside of the rocket body to an outside thereof.
Opening claim text (preview).
What is claimed is: 1. A rocket for artificial rainfall using an ejection hygroscopic flare, the rocket comprising: a rocket body configured to descend with a parachute after flight by thrust, and having a hygroscopic flare discharge outlet; a communication module installed in the rocket body, and configured to transmit and receive a launch command and an ejection command with a ground station; an ejection hygroscopic flare installed in the rocket body and filled with cloud seeds and a burning material therein; and a hygroscopic flare ejection device configured to separate and eject the ejection hygroscopic flare from an inside of the rocket body to an outside thereof. 2. The rocket of claim 1 , wherein the ejection hygroscopic flare comprises: a cylindrical hygroscopic flare body with an open end; and a cover coupled to the open end of the hygroscopic flare body, wherein a plurality of discharge holes are formed along an outer circumference of the hygroscopic flare body. 3. The rocket of claim 2 , wherein the hygroscopic flare body comprises a main chamber and an extension chamber connected to the main chamber, wherein the main chamber comprises a bottom portion, a cylindrical outer portion connected to the bottom portion, and a coupling flange extended from an end of the outer portion and connected and coupled to the extension chamber; and wherein the extension chamber has a cylindrical structure, with opposite ends from each of which a coupling flange is extended.
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