FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed flight vehicle comprises power plant, fuselage and wing fragments. Set of wing fragments comprises bearing and control surfaces and their mounts. Wing fragment includes structural set including spar, stringer and ribs. Fuselage includes set of frames, spars, stringers and skin. Frames and spars have opening to fasten wing fragments. Engine reversing device comprises flap pivoted in housing to close its openings and provided with grids composed of gas flow guide vanes. Air intake with jet engine integrated in fuselage tail features variable-depth grooves arranged opposite each other on supports. Control system comprises control rod with pedals at its bottom and handle at its top. Said handle has landing gear extension/retraction knob and that of electric drive of bottom set of fragments. Methods of flight vehicle control comprise exploiting air and gas flows.
EFFECT: simplified servicing.
47 cl, 30 dwg
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