发明名称 MISSILE LAUNCHING POD
摘要 FIELD: rocketry; devices for missiles launching. ^ SUBSTANCE: the invention is pertaining to the field of weapons, in particular, to devices for missiles launching and may be used for production of the missile launching pods, predominantly of a hermetic type. The missile launching pod safety stopper is made out of a wedge-shaped plate-shell, on the front narrow end of which there is a coupling device for a support element of the missile. At the rear end there are at least two fastening tools made in the form of the radial bolts, which have been screwed in the mushroom-shaped lugs fixed in a pipe wall and pressed by outside screw nuts. The heads of the mushroom-shaped lugs are conjugated with along the conical set to the holes made in a shell, and the shell is located in the wedge-shaped outcaliber pit of the pipe cavity. Lateral surfaces of the pit are made with the return bevel forming with a shell a coupling of the "dovetail"-type. Realization of the invention will ensure the improved reliability of operation, hermiticity of the missile launching pod and reduction of its overall dimensions due to location of the stopper in the pit of the pipe cavity. ^ EFFECT: the invention ensures the improved reliability of operation, hermiticity of the missile launching pod and reduction of its overall dimensions. ^ 3 dwg
申请公布号 RU2263868(C1) 申请公布日期 2005.11.10
申请号 RU20040128480 申请日期 2004.09.28
申请人 发明人 MAKAROVETS N.A.;SEMILET V.V.;BARYNIN V.A.;KUL'KOV A.A.;PLOTNIKOV V.I.;JAIKOV V.P.;LUK'JANENKO V.S.;PUKHOV A.A.;TIMAKOV A.M.
分类号 F41F3/042 主分类号 F41F3/042
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