FIELD: transportation.
SUBSTANCE: hemispherical canopy of a parachute is implemented with vent, above of which is fixed reflecting barrier. Barrier is implemented with spouts, free ends of which are located in aerodynamic darkening area. Additional polar beckets are passed through holes in polar part of canopy and fixed on barrier. Total area of spouts cross sections is accepted as equal to cross section of polar vent.
EFFECT: loss of parachute coming down speed and operation improvement.
2 dwg
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