| 摘要 |
FIELD: defensive weapon. SUBSTANCE: to increase overloads without worsening the aerodynamic characteristics, an additional part of the control fin is formed in the zone of the tip chord at an angle relative to the longitudinal axis. It allows to increase the control fin span and at the same time to provide control fin folding within the space between the inside diameter of the pipe- container and the body of the control actuator block. A pylon made in the form of a T-shaped plate is installed on the body of the control actuator block before the control fin. The pylon provides for a smooth, without any stall, flow past of the control fin by aerodynamic flow and for an increase of the control fin angle, which, in turn, provides for an increase of the developed moment of the control actuator block. EFFECT: enhanced effectiveness of missile control. |
