FIELD: armament, in particular, guided missiles.
SUBSTANCE: the guided missile has a body with on-board systems, frame with drive shafts made with journals, with air vanes hinge-installed in their end face grooves for folding in the body and fixation in the unfolded position. The guided missile is provided with control-surface deflection transducers and a printed circuit board secured through an insulator on the front end face of the frame and connected by means of a bundled conductor to the on-board systems of the guided missile.
EFFECT: reduced spread in the value of the sweep angle of the air vanes in the process of manufacture.
2 dwg
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RU2669979C1 |
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Authors
Dates
2005-01-20—Published
2003-07-08—Filed