Launching method of guided missile safe launching system

Abstract

The invention provides a launching method of a guided missile safe launching system. The safe launching system comprises a launching control system and a launching box / barrel. The launching control system comprises an ignition power source and a launching control unit. The launching control unit comprises a combat launching command relay, an engine ignition relay and a resistor. The launching box / barrel comprises a napalm bomb mechanism microswitch. After an initiating explosive device is connected with the resistor in parallel, one end of the circuit is sequentially connected with the napalm bomb mechanism microswitch, a first set of contact switches of the engine ignition relay and a first set of contact switches of the combat launching command relay in series; the other end of the circuit is grounded and then is sequentially connected with a second set of contact switches of the engine ignition relay and a second set of contact switches of the combat launching command relay in series. According to the safe launching system, the safety performance in missile launching can be improved.

Description

technical field [0001] The invention relates to the field of missile launching, in particular to a launching method of a missile safety launching system. Background technique [0002] During the development and use of anti-aircraft missile weapon system, safety has always been an important work content. Safety first is unquestionable in the development and use of weapons and equipment. Security is an inherent attribute of a weapon system and a prerequisite for ensuring safe use. Improving product safety and ensuring safety are the primary requirements for the development, production, use and support of missile weapons and equipment. High safety is one of the important factors to ensure the effectiveness of weapons and equipment. The missile safety is the core item in the missile weapon system security, and the engine safety during the missile launching process is the core item of the missile weapon system security. [0003] In addition, the weapon firepower density of we...

AI Technical Summary

Problems solved by technology

[0004] The problem solved by the present invention is that the existing missile launch safety and reliability index requirements are constantly increasing, and the original design does not meet the design requirements. In order to solve the above problems, the present invention proposes a missile launch system with high safety and reliability. method

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