FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to VTOL compact unmanned aerial vehicles. Combat multicopter with cumulative projectile includes a bearing part having bladed rotors with their rotation drives connected to the housing, an accumulator, a remote control system, a video camera and a warhead equipped with a cumulative projectile. Bearing part is made on the basis of multicopter weighing not more than one kilogram. Warhead is equipped with a sealed plastic casing installed in the lower zone of the housing of the bearing part with the possibility of disconnection. At least one cumulative charge weighing not more than 460 grams is installed in a sealed plastic casing. Warhead is equipped with a check valve, an electric detonator, a detonating cord and a control controller with a power element, which are connected to a cumulative charge. Combat multicopter remote control system is equipped with a receiving-transmitting device connected to the combat unit control controller. Total weight of the warhead does not exceed 700 grams.
EFFECT: reduced weight and dimensions, increased manoeuvrability, efficiency of target destruction.
2 cl, 4 dwg, 1 tbl
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Authors
Dates
2024-05-02—Published
2023-08-27—Filed