FIELD: military equipment, artillery ammunition. SUBSTANCE: ballistic cap uses a hollow casing fastened on the missile top by destructible members, the casing accommodates the remote-control launch device and the separation device made in the form of a piston installed with formation of an annular cavity between its front end and hollow casing. The piston has an afterburner with a propellant charge and electric fuze eccentrically arranged and communicating with the annular cavity, the electric fuze is electrically connected to the remote - control launch device. The afterburner outlet is closed with a blowout diaphragm, and a groove is made in the top of the hollow casing to receive an annular stop screwed in the piston. EFFECT: improved design. 1 dwg
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Authors
Dates
1997-09-10—Published
1995-01-17—Filed