FIELD: flying vehicle control units. SUBSTANCE: proposed device includes hollow aerodynamic needle mounted in nose section of flying vehicle which is provided with radial openings for transversal blowing-off of jets; device is also provided with air intakes mounted on lateral surface of nose section of flying vehicle for radial motion; they are connected with cavity of fixed aerodynamic needle by means of flow- through passage; aerodynamic needle has closed front portion and is provided with heat- insulated coat. EFFECT: enhanced efficiency of around-aircraft flow control at supersonic and hypersonic flights. 2 cl, 2 dwg
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