FIELD: aviation.
SUBSTANCE: method of control of aerodynamic characteristics of supersonic aircrafts includes installation of flat MHD-generators in pairs symmetrically with reference to the plane of symmetry of elements of fin assembly of hypersonic aircrafts (HSA), and between them the magnetoshielding plates are placed which are made of ferromagnetic material with a Curie point exceeding the working temperature of HSA elements ensuring stability, controllability and balancing. The control commands from the onboard control system are supplied to solenoids of flat MHD-generators located under that streamline surface of fin assembly elements of HSA which is effected by the control force. The magnetoshielding plate is made of cobalt.
EFFECT: expansion of functional capabilities of HSA control via pitch, roving and list channels.
2 cl, 4 dwg
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