FIELD: transport.
SUBSTANCE: invention relates to aircrafts and concerns aerodynamic configuration of unmanned aitcrafts. Modular unmanned aircraft contains body 1 of elongated form with carrying beam 2 positioned along the body 1. Suspension assemblies 3,4 are set on carrying beam 2 where rear suspension assembly 4 is combined with swivel block 6 of wing 7 of the aircraft. Semispan of the wing 7 is less than or equal to the distance between suspension assemblies 3, 4.
EFFECT: increase in reliability of start and deployment of modular unmanned aircraft wing, increase in efficiency of armament section due to better control of its opening.
3 dwg
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