| 摘要 |
FIELD: aeronautical engineering. SUBSTANCE: at definite moment, cylindrical panels of mating compartments of flying vehicle open due to extension of rods 6 of drives 7, thus changing geometry of mating compartments. Angle of opening of cylindrical panels of mating compartments in part of flying vehicle which continues flight is lesser than angle of opening of cylindrical panels 3 in part of flying vehicle which has completed its functioning. Lattice surface of cylindrical panels is formed by longitudinal fixed plates 9 and transverse swivel plates 10 which are connected with flying vehicle case by means of rods. As cylindrical panels are opening, transverse plates 10 turn and get oriented in flight at zero angle of attack, thus providing for static aerodynamic stability and impactless separation of parts of flying vehicle and reducing the mass of structural members of separation system and overall dimensions of flying vehicle case. EFFECT: static aerodynamic stability of flying vehicle in dense atmosphere; avoidance of pursuit and collision of part which has completed its functioning and that which continues its flight. |
