FIELD: flying vehicle equipment. SUBSTANCE: proposed facility includes parachute for stabilization of flying vehicle position, parachute for reduction of horizontal and vertical components of flying vehicle speed, rocket secured after canopy of parachute used for reduction of horizontal and vertical components of flying vehicle speed and two ropes; one rope is connected with shroud lines of parachute used for reduction of horizontal and vertical components of flying vehicle speed. Provision is also made for rope heaving-in unit mounted inside case. Second rope is connected with shroud lines of parachute used for stabilization of flying vehicle position. Provision is also made for two additional ropes whose ends are secured on rope connected with parachute used for stabilization of flying vehicle position and with case at point of connection with outer wing panels. EFFECT: enhanced reliability in emergency situations. 2 cl, 6 dwg
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Authors
Dates
2002-10-20—Published
2001-03-29—Filed