FIELD: aeronautical engineering. SUBSTANCE: proposed system includes canopy with main lines, control lines with two branches at one end which are secured to main line, strip with rings through which lines are passed, auxiliary parachute connected with strip. Provision is also made decelerator including bearing member and coupling system. Bearing member has shape of square with rings at corners and platform with foot rest on inner surface. Coupling system includes band with rings and elastic cords with spring hooks at the ends. Bearing member has bend. Each elastic cord is fastened to band ring by one spring hook and to ring of bearing member by other spring hook; band is passed through loops of lift webs. EFFECT: extended technological capabilities. 1 dwg
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Authors
Dates
2003-05-27—Published
2001-06-13—Filed