Full-state air-to-air missile front cabin air pressure test device

An air-to-air missile, all-state technology, applied in the direction of ammunition testing, ammunition, weapon accessories, etc., to meet the structural and economical effects

Inactive Publication Date: 2009-11-18
CHINA AIR TO AIR MISSILE INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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  • Full-state air-to-air missile front cabin air pressure test device

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[0007] The present invention will be described in further detail below. Referring to Fig. 1, the high voltage test device of the present invention includes carrier 1 and

The launching device 2 connected with the carrier aircraft. The circuit box 8 installed in the launcher 2 is connected to the frame connector 7 through a cable

Connection, at the same time, the circuit box 8 is connected with the separation plug 5 fixed on the launcher 2 through a cable, and the separation plug 5 is connected with the installation

The separation socket 6 on the front compartment of the tested air-to-air missile is plugged and connected. It is characterized in that there is a

The simulated engine cabin section connected to the cabin, the shape, stiffness, strength, center of mass, suspension mechanism and missile front cabin of the cabin section

The connection structure is the same as that of the real engine compartment. Connect a simulated steering gear compartment to the rear of the ...

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Abstract

The invention belongs to the air-to-air missile system test technology, and relates to a device for air testing the front cabin of the full-state air-to-air missile, in particular to a high-pressure test device for the front cabin of the full-state air-to-air missile. Cable connectors and cables were installed on the original launching device, and a 57-volt power supply was installed on the simulated rear missile body, so that the aircraft, the front cabin of the missile and the 57-volt power supply established a second-level functional connection except for the launch control function. The invention can carry out the interception and tracking test of the real target by the front cabin of the air missile without changing the composition and technical state of the front cabin of the active radar guided air-to-air missile before launch.

Description

Technical Field The invention belongs to air-to-air missile system test technique, relate to a kind of air-to-air missile front cabin to full state air-to-air missile A device for testing, in particular to a device for applying high pressure in the air to the front cabin of a full-state air-to-air missile. Background technique Active radar type air-to-air missile in the development process is before target test, whether it still has quality through static test In particular, there are still many uncertainties about whether the real target can be reliably guided after launch. Step by step according to the test The principle of advancement, puts forward the state in the air before launch, without changing the composition and technology of the front cabin of the active radar-guided air-to-air missile State (including hot battery), the need to conduct interception and tracking experiments on real targets. While carrying out the above test, it is necessary to solve the pr...

Claims

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Application Information

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IPC IPC(8): F42B35/00F41G7/00
Inventor 刘未学徐和仁
Owner CHINA AIR TO AIR MISSILE INST
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