FIELD: aviation.
SUBSTANCE: invention relates to unmanned aerial vehicles. Portable folding installation for ejection of small-size UAV contains a beam consisting of front (1) and rear (2) beams, having longitudinal guide slots. Longitudinal beam is equipped with frame structure (65) intended for opening of fixing locks (64). Front support (5) is made of front posts (7) fixed on the support connected to the base pipe, on which the aircraft brake shock-absorbing cord (12) with termination assemblies (14) is located, as well as roller mechanism (13) of starting and braking shock-absorbing aircraft cords. Rear support (21) is made in the form of inclined tubular post connected to rear beam (2) by means of channels. Bogie is made in the form of carriage (10) equipped with starting shock-absorbing aircraft cord, fixing locks, lodgments (17), starting lock and thrust brackets for UAV fixation.
EFFECT: simplification of the design is achieved.
1 cl, 12 dwg
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