FIELD: aircraft engineering.
SUBSTANCE: proposed procedure consists in application of powder engine. Note here that said engine is actuated by electric signal from transducer subject to current altitude, pilot weight and pilot parachute landing vertical speed. Proposed system is arranged and catapult seat bottom surface. It consists of four-nozzle powder engine with minimum possible operating time and optimum direction of thrust and altitude-and-vertical speed transducer direction, transducer outputting engine actuation instruction subject to current altitude, pilot weight and pilot parachute landing vertical speed. Pilot weight data is received by said transducer from seat ACS at ejection.
EFFECT: decreased speed after ejection.
2 cl, 2 dwg
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