FIELD: weapons.
SUBSTANCE: invention relates to weapons and can be used in determining accuracy of missile weapons systems of long storage life. Proposed method comprises determination of main flight characteristics of guided sea missiles taking into account their storage life. For long-term storage of a missile, up to 40 years and more, the degree of depletion of the powder charge of the starting engine - incompleteness of its burning is taken into account. Change of main flight characteristics at the end of trajectory starting section is determined from this parameter. At that, for anti-aircraft guided missile flight characteristics are determined by one analytical expression, and for cruise missile - by another analytical expression.
EFFECT: technical result is higher efficiency of using missile systems when firing at a given target.
1 cl, 15 dwg
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