FIELD: transport.
SUBSTANCE: invention relates to aircraft catapult launchers. Proposed method comprises using a combined gas-fluid chamber interacting with gas cylinder and control valve making a launching complex, forcing gas from gas cylinder into the chamber gas receiving assy via control valve, simultaneous pushing of all rows of pistons in said fluid receiving assy of the chamber and launching the weight at constant power. Proposed device comprises gas cylinder, control valve and combined gas-fluid chamber. High-power gas tank is connected with said gas cylinder to feed power. Said gas cylinder is connected with gas receiving assy of said combined gas-fluid chamber via control valve and pipe. Power regeneration device comprises lifting cylinder, transfer trolley, transducer, damping cylinder and guide bar.
EFFECT: lower power consumption.
10 cl, 3 dwg
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