FIELD: weapons and ammunition.
SUBSTANCE: method for installation of missile stabilising device empennage blades includes assembly of empennage with rigidly fixed blades on vessel at the specified working angle of blade inclination, measurement and calculation of actual working angle of inclination of each installed blade. Discrepancy of actual and specified working angles of missile stabilising device empennage blades inclination is compensated due to arrangement of levelling site with specified width at surface of each blade, and its determining linear size is calculated according to the given formula.
EFFECT: invention maintains specified mode of missile rotation.
2 cl, 2 dwg
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