FLYING VEHICLE SPIN RECOVERY SYSTEM Russian patent published in 2001 - IPC

FIELD: flying vehicle equipment. SUBSTANCE: proposed system includes container made in form of pipe with one open end which is mounted in tail section of fuselage. Container is provided with parachute unit including main and auxiliary parachutes. Cover of auxiliary parachute is connected with store jettisoning mechanism. Provision is made for adapter unit located in guide longitudinal passage and connected with main parachute and with load-bearing attachment unit through shorter load- bearing member of parachute unit and cutter. Container is divided lengthwise into compartments by walls-diaphragms for arrangement of system units. Parachute unit is arranged in tail compartment. Adapter unit is made in form of solid H- shaped body with holes over its edges through which axles are passed. Main parachute is connected with one of them and shorter load-bearing member of parachute unit is connected with other axle. Located in form section of guide longitudinal passage is stop rigidly secured in base of wall-diaphragm for limiting longitudinal motion of adapter unit. Cutter is made in form of plasma gas generator units located in succession and secured in center compartment on transversal walls-diaphragms. Load-bearing attachment unit is fixed in front compartment of container. EFFECT: reduced overall dimensions and mass; enhanced operational safety. 3 cl, 3 dwg