FIELD: weapons.
SUBSTANCE: invention relates to ammunition, namely to design of unguided aircraft missiles. Unguided aircraft missile comprises a high-explosive fragmentation warhead of a penetrating type, a rocket part with folding blades and a head mechanical double-mode fuse. Warhead body is cylindrical and has a truncated cone end with smaller diameter d equal to 0.79–0.82 and height h equal to 0.58–0.61 of calibre D of the warhead. Axes of folding blades of the rocket part are located on the diameter d1, which is in range of 0.84–0.87 of calibre D1 of the rocket.
EFFECT: invention increases efficiency of using unguided aircraft missiles.
1 cl, 1 dwg
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Authors
Dates
2024-11-05—Published
2023-05-25—Filed