FIELD: rocketry, applicable in small-sized complexes of various purpose.
SUBSTANCE: the missile nose cone is made detachable in the longitudinal axis of lugs and installed on the base in the form of a tube having two coaxial tapered holes through which the waveguides of the antenna launching branch are passed. Installed in the aft part of the missile at the front end face of the tube is a screen for protection of the antenna device of the launching branch.
EFFECT: enhanced reliability of operation, reduced aerodynamic drag at the launching leg of the trajectory and simplified process of assembly.
3 dwg
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Authors
Dates
2005-06-27—Published
2003-11-06—Filed