FIELD: armaments and ammunition.
SUBSTANCE: device of missile stabilization contains controls in form of four pairs kinematically linked with each other, and pair of ribbon tie-rods tensioned by turnbuckle with rollers of aerodynamic and gas vanes with shafts having slot for bushing, ring groove with wire passing through the rollers, rocker pivotally connected with pair of ribbon tie-rods.
EFFECT: invention reduces device dimensions.
4 dwg
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Authors
Dates
2015-11-20—Published
2014-10-22—Filed