FIELD: flying vehicles launched from stationary and mobile sets including submarines. SUBSTANCE: high-pressure cavities are filled with working gas after which mains running to flying vehicle systems are opened; generation of working gas and filling of cavities shall be performed simultaneously. Both procedures are started immediately before launch. System contains high- pressure working gas sources connected with units and systems of flying vehicle by means of mains; system includes also flying vehicle launch control unit. Working gas source is made in form of solid propellant generator of cold pure nitrogen. Generators are located on separable members of flying vehicle; launching devices are connected with flying vehicle launch control unit. EFFECT: improved mass and dimensional characteristics; enhanced reliability and safety of operation due to avoidance of high-pressure bottles. 3 cl, 3 dwg
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Authors
Dates
2000-04-27—Published
1999-07-02—Filed