FIELD: transport.
SUBSTANCE: set of inventions relates to aerostatic flight vehicles. In compliance with first version, this method consists in installation of transporter-launcher container along aircraft fuselage. Said container has opening for payload exit and guides that make air chamber at cavity front part. Gas jets are forced into said air chamber from high-pressure source. After partial forward-displacement of payload second gas jet is forced into air chamber. Flow rate of first jet and combined flow rate of first and second jets are set proceeding from pressure constriction inside transporter-launcher carrier. In compliance with second version, second gas jet is forced from extra high-pressure source.
EFFECT: accelerated dropping of payload without increased in container weight, maximum lengthwise overload.
2 cl, 2 dwg
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