FIELD: aeronautical engineering. SUBSTANCE: launch complex includes semi-fuselage carrier aircraft which has at least two fuselages located at some distance relative to each other, flying vehicle to be launched and supports intended for placing the vehicle to be launched. Supports for placing the above-mentioned vehicle on carrier aircraft are provided with guides which are located at the top relative to fuselages along their longitudinal axes. One support is provided with its own engine plants and rollers. EFFECT: improved aerodynamic characteristics. 4 cl, 4 dwg
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