FIELD: military equipment, in particular, aerodynamic stabilizer of spin-stabilized missile. SUBSTANCE: the stabilizer unit has a fairing and arched blades installed in the fairing on supports for rotation on axles, turned at an angle to the fairing generating line, the generating line of each blade is turned relative to its root chord, the angle of turn is positive and equals the angle of turn of the axle, and the blades are installed for opening in the direction of turn of the axles, the front support of the blade is removed from the front edge of the blade is removed from the front edge of the blade at a distance not exceeding 0.15 of the length of the root chord. EFFECT: enhanced aerodynamic efficiency of the stabilizer, with the unit dimensional characteristics remaining unchanged. 3 dwg _
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Authors
Dates
2002-04-20—Published
2001-08-08—Filed