Cartridge stern and assembling method of cartridge stern

Abstract

The invention provides a cartridge stern and an assembling method of the cartridge stern. The cartridge stern comprises a shell, a satellite measurement module, an electronic cabin module, multiple pulse engines, and an energy cabin module; the shell comprises a body, an electronic cabin cavity, an energy cabin cavity, a plurality of mounting cavities and an antenna mounting groove, wherein the electronic cabin cavity, the energy cabin cavity and the mounting cavities are formed in the end face of the body, and the antenna mounting groove is formed in the circumferential side wall of the body; the satellite measurement module comprises an antenna circuit board located in the antenna mounting groove and a satellite receiver arranged on the antenna circuit board; the electronic cabin module is in control connection with the satellite measurement module; the multiple pulse engines and the multiple mounting cavities are correspondingly arranged, and the electronic cabin module controls the pulse engines to ignite according to signals transmitted by the satellite receiver; and the energy cabin module is located in the energy cabin cavity, and the satellite measurement module and the electronic cabin module are electrically connected with the energy cabin module, so that the satellite measurement module, the electronic cabin module, the multiple pulse engines, the energy cabin module and the shell form a modular structure. The cartridge stern provided by the technical schemes of the invention can form a modular structure, so that the assembly efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of guided shells, in particular to a shell stern and a method for assembling the shell stern. Background technique [0002] Conventional guided shells refer to the use of large-caliber barrel artillery to launch, and the use of comprehensive range-extending technologies (rocket-assisted range-extending, bottom row drag-reducing range-extending, gliding range-extending, etc.) to achieve a longer range; Jet flow control or aerodynamic surface control technology enables higher precision; modular warhead technology is used to complete shells for different combat tasks. [0003] In the prior art, the electronic cabin, the energy cabin and the satellite receiver of the guided shell are dispersedly arranged in the projectile body or the fuze of the guided shell. Such a dispersed structure is not convenient for the assembly of the guided shell and will reduce the assembly efficiency of the shell. Contents of the i...

AI Technical Summary

Problems solved by technology

[0003] In the prior art, the electronic cabin, energy cabin and satellite receiver of the guided projectile are dispersedly arranged in the projectile body or fuze of the guided projectile, such a dispersed structure is not convenient for the assembly of the guided projectile, and will reduce the assembly efficiency of the projectile

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