| 摘要 |
FIELD: aeronautical engineering. SUBSTANCE: seat includes seat proper, head-rest with stabilizing rods with life-saving parachute inside it, ejection gun, one main and two auxiliary powder rocket engines mounted on rear surface of head-rest, seat automatic control system consisting of ejection seat stroke sensor, baroswitch, meter for determination of acceleration along longitudinal axis; control system provides for determination of functional configuration of seat on basis of information on mode and parameters of flight of aircraft. EFFECT: high safety of ejection. 2 dwgs
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