FIELD: weaponry.
SUBSTANCE: invention relates to weapons and can be used in self-guided missiles. The proposed missile comprises a detachable nose unit and self-guidance head, both being fitted with fairings, air-dynamic steering drive furnished with air intake and central bore in the nose unit fairing. The missile is provided with sealing circular adapter inserted in the clearance between the fairings and fixed on the nose unit. The proposed method comprises the jobs of mounting and fixing the steering drive, self-guidance head, nose unit and fairings.
EFFECT: improved manufacturability.
2 dwg, 2 cl
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