An anti-aircraft system is described and includes an unmanned aerial vehicle (UAV) comprising a body; a wing connected to the body; and propulsion systems associated with the wing, wherein the propulsion systems comprise pylons releasably connected to opposite ends of the wing such that the propulsion systems may be selectively released from the wing during flight of the UAV.
UNMANNED AERIAL VEHICLE FOR ANTI-AIRCRAFT APPLICATIONS
2022-05-12
Patent
Electronic Resource
English
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