Drone launching system and method of using a drone launching system

Abstract

A drone propellant system mounted on an unmanned aerial vehicle (UAV) consists of a body and a housing (11), inside which a net (10) is placed. The system is characterized in that the body consists of a high-pressure chamber module (1) and a low-pressure chamber module (5). A propellant charge (2) with an ignition device (3) is placed in the high-pressure module (1). Gases flow between them through an opening (6). In addition, barrel openings (13) are made in the low-pressure chamber – at an acute angle – to the system's axis of symmetry. The method of using a drone propellant system mounted on an UAV involves firing a net (10). This method involves inserting a propellant charge (2) with an ignition device (3) into the high-pressure chamber (1), and inserting a net (10) connected to weights (projectiles) (8) into the housing (11), followed by activating the ignition device (3).