FIELD: aviation.
SUBSTANCE: projectile includes a body, in the middle of which a warhead with an explosive charge is installed. A stabilizer is installed on the back of the case. The warhead of the projectile has a compartment with tanks for the combustible component and the explosive oxidizer. The reservoirs are connected through gas supply nozzles to a gas generator with a starting device installed in the front part of the projectile body. A membrane is installed in each tank, designed to break when gas flows from a gas generator with a starting device through tanks with fuel and oxidizing components. The reservoir compartment is connected through a nozzle and a diffuser with an elastic shell located in the rear part of the projectile body and made with the possibility of filling with an explosive mixture aerosol formed by mixing a combustible component and an explosive oxidizer in the elastic shell, for detonation of which a fuse is installed in the rear part of the projectile body with a time mechanism.
EFFECT: increase of efficiency of aircraft projectiles and volumetric detonating ammunition in open space.
1 cl, 4 dwg
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Authors
Dates
2023-04-13—Published
2022-04-11—Filed