Missile performance testing unit for missile testing system

Abstract

The invention discloses a missile performance testing unit for a missile testing system, and relates to the technical field of missile testing devices. The missile performance testing unit comprises amissile performance testing unit box body, a second alternating current input interface is embedded in the missile performance testing unit box body, and the second alternating current input interface is connected with one power supply input end of a first DC-DC conversion circuit through a second power supply switch and a second switch power supply, the first path of the output end of the firstDC-DC conversion circuit is connected with the input end of a second power supply processing circuit, the second path of the output end of the first DC-DC conversion circuit is connected with the power input end of a cranking module, and a second direct current power socket is embedded in a turntable control unit box body. The missile performance test is completed by matching a computer measurement and control unit, a turntable control unit, the missile performance testing unit and an air source component, and the missile fault diagnosis rate and maintenance efficiency can be improved.

Description

technical field [0001] The invention relates to the technical field of missile testing devices, in particular to a missile performance testing unit for a missile testing system. Background technique [0002] The missile ground test device is to conduct a comprehensive functional inspection and monitoring of the various subsystems and the overall system of the missile before the missile is launched, set the flight parameters, and put the missile in a standby state. Although the missile has undergone a comprehensive and detailed unit test and comprehensive test before launch, in order to ensure the reliable and safe launch of the missile, a test is still required after entering the launch site, but the test items should be few and precise. The main key inspection items include the inspection of the power supply system on the bomb, the inspection of the ignition path of the pyrotechnic product, the inspection of the path resistance, the ignition sequence test and the dynamic te...

AI Technical Summary

Problems solved by technology

[0003] The early missile ground comprehensive test system used manual test or semi-automatic test. The disadvantages are that the test system is large in size, poor in portability, complex in the test process, requires more equipment, requires human participation, low efficiency, and the interval between test and launch control. Long, and the distance between people and the missile under test is relatively close, which poses a safety hazard

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