| 摘要 |
FIELD: armament. ^ SUBSTANCE: the guided missile, having a canard aerodynamic configuration, has a cylindrical body, stabilizer and aerodynamic control surfaces. A circular pylon made of a ring plate coupled to the body by plane-surface plates in installed on the body nose before the control surface. According to the other modification, a plane-surface pylon made of plates cantilever fastened an the body at an angle of 45 deg. relative to the plane of the control surface cantilevers is installed on the guided missile nose behind the control surface. ^ EFFECT: enhanced efficiency of the guided missile. ^ 2 cl, 8 dwg |
