FIELD: flying vehicles. SUBSTANCE: control member consists of all-moving panel 1 provided with movable nose portion 3 made for deflection through angle of ± 90° relative to on-board chord 6. EFFECT: reduction of power requirement of power plant of control system through reduction of hinge moments of all-moving panel of tail unit at supersonic speeds. 2 cl, 3 dwg
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Authors
Dates
1995-07-25—Published
1991-06-07—Filed