Launching Method of Missile Safety Launching System

A launch system and missile technology, which is applied in the launch field of the missile safety launch system, can solve problems such as not meeting the design requirements, and achieve the effects of avoiding static electricity accumulation, ensuring safety, and reducing induced current

Active Publication Date: 2016-08-17
SHANGHAI INST OF ELECTROMECHANICAL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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  • Launching Method of Missile Safety Launching System
  • Launching Method of Missile Safety Launching System

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Embodiment Construction

[0022] Hereinafter, the present invention will be further described with reference to the accompanying drawings and embodiments.

[0023] refer to figure 1 , the missile safety launch system provided by the present invention includes:

[0024] Launch control system 01, launch box / tube 02; the launch control system 01 includes an ignition power supply 011 and a launch control unit 012, and the launch control unit 012 includes a combat launch order relay 0121, an engine ignition relay 0122, and a resistor 0123; the The launch box / canister 02 includes a microswitch of the fixing mechanism; after the pyrotechnic product of the missile 03 is connected in parallel with the resistor 0123, one end of the microswitch of the fixing mechanism and the first group of contact switches of the engine ignition relay 0122 are connected in series in sequence. , The first group of contact switches of the combat firing order relay 0121; the other end is grounded, and the second group of contact s...

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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 launch, in particular to a launch method of a missile safety launch system. Background technique [0002] In the development and use of air defense missile weapon systems, security has always been an important work content. Safety first, there is no doubt 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, and high safety is one of the important factors to ensure the effectiveness of weapons and equipment. Missile safety is the core item in the safety of missile weapon system, and engine safety during missile launch is the core item of missile weapon system safety. [0003] In addition, the weapon firepower density of the weapon system is also getting high...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F41F5/00
Inventor 陈本军李加宝李颖范文晶赵伟忠周黎敏孙刚叶智明高方军黄志立
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG
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