FIELD: weapons and ammunition.
SUBSTANCE: invention relates to airborne weapons, particularly, to the "Block"-type multibarrel missile launchers. This launcher comprises the cylindrical pipe 1, front and rear cowls 2, 3, launcher pipes 6, gas discharge pipes 7 arranged parallel with the latter, one per every launcher pipe, and disposable composite web 11. Tail section of every pipe 7 is located ahead of appropriate segment slit 15. Said slit 15 is arranged at the gate to turn the missile jet stream through 180 degrees and to feed it into gas discharge pipe 7 and, further, to appropriate section of heatproof web 11. Said design allows the pre-breakage of said web arranged ahead of the missile so that optics located at the head of missile is not damaged.
EFFECT: efficient launching of missiles with optical, electronic and laser instruments built in their heads.
2 cl, 6 dwg
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Authors
Dates
2015-12-27—Published
2013-11-07—Filed