FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to systems for launching of unmanned aerial vehicles from aircraft carriers. Unmanned aerial vehicle comprises units for fixation on launching device of carrier aircraft, acceleration propulsion system, control system of its position in autonomous flight, payload, as well as pulse jet engines for creation of rotation pulse around transverse axis passing through gravity center of unmanned aerial vehicle, with pitch angle increase, and compensation of this rotation pulse. UAV is equipped with braking parachute, which comprises canopy, rope and slings connecting canopy with rope. UAV is equipped with a box fixed on the UAV from the tail part through the box fixing device, configured to unfix its attachment, and a device for fixing the end section of the cable in the zone of the upper point of the surface of the tail part, configured to unfix the attachment. Canopy, slings and initial section of rope are packed in box, and final section of parachute rope is fixed in its attachment device.
EFFECT: reduced weight of unmanned aerial vehicle and time of its launching to altitude flight path.
1 cl, 6 dwg
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Authors
Dates
2020-07-23—Published
2020-02-17—Filed