FIELD: aeronautical engineering.
SUBSTANCE: according to first version, proposed system includes containers for stowage in non-operating state which are located in upper and lower parts of flying vehicle. Proposed system includes also modules of set of inflatable envelopes, subsystem for drawing the inflatable envelopes and placing them in operating position, subsystem for control of pressure inside envelopes, subsystem for placing the envelopes in non-operating position. System is also provided with reinforced inflatable devices located on sides of flying vehicle and nozzles for escape of gas jet from gas generator. According to second version, proposed system is additionally provided with disintegration facilities and subsystem for separation of fuselage into autonomous compartments.
EFFECT: enhanced reliability and fast speed of response.
33 cl, 8 dwg
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