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Detonating control system for initiating explosive device and test method thereof

A technology of control system and pyrotechnics, which is applied in the aerospace field, can solve problems such as insufficient testing of pyrotechnics, limited test safety of pyrotechnics detonation control system, test site, and difficult measurement

Active Publication Date: 2020-07-10
INNOVATION ACAD FOR MICROSATELLITES OF CAS +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The existing pyrotechnic detonation control system is limited by the test safety and test site, and it is difficult to carry out large-scale double-wing sailboard deployment operation, and the single wings need to be deployed separately. Therefore, it is necessary to improve the reliability and safety of pyrotechnics; in addition, aerospace It is generally difficult to carry out the final measurement before launching the arrow into the launch tower, which makes the test of pyrotechnics insufficient

Method used

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  • Detonating control system for initiating explosive device and test method thereof
  • Detonating control system for initiating explosive device and test method thereof
  • Detonating control system for initiating explosive device and test method thereof

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Embodiment Construction

[0038] In the following description, the present invention is described with reference to various examples. One skilled in the art will recognize, however, that the various embodiments may be practiced without one or more of the specific details, or with other alternative and / or additional methods, materials, or components. In other instances, well-known structures, materials, or operations are not shown or described in detail so as not to obscure the inventive concepts of the present invention. Similarly, for purposes of explanation, specific quantities, materials and configurations are set forth in order to provide a thorough understanding of embodiments of the invention. However, the invention is not limited to these specific details. Furthermore, it should be understood that the embodiments shown in the drawings are illustrative representations and are not necessarily drawn to correct scale.

[0039] In this specification, reference to "one embodiment" or "the embodiment...

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Abstract

The invention discloses a detonating control system for an initiating explosive device, thereby realizing controlling of detonating of an initiating explosive device by three-level control. The control system comprises a control circuit and a protection and measurement system. The control circuit comprises a first relay, a second relay, a third relay, a current-limiting resistor, a casing ground,a bleeder resistor for discharging static electricity, and a protection and measurement system; the first relay protection and measurement system, the second relay and the third relay are used for controlling on-off of a circuit; the current-limiting resistor is connected with the relays in series; and the protection and measurement system comprises a plurality of star catalogue sockets. The connection and disconnection of an initiating explosive device control circuit can be controlled by plugging protection plugs or emission plugs into the star catalogue sockets, and an initiating explosivedevice detonating loop, a detonating time sequence and a bridge wire resistance value can be measured for many times at any stage.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to an explosive detonation control system and a testing method thereof. Background technique [0002] The pyrotechnic device is a sailboard deployment separation detonation device commonly used on spacecraft. After the spacecraft enters orbit, it first needs to detonate the sailboard pyrotechnic device to realize the unlocking of the mechanism, the deployment of the solar panel, and supply energy for the spacecraft. [0003] Usually, before the launch of the spacecraft, a large-scale sail panel deployment test will be carried out to verify the correctness of the design of the explosive detonation circuit. Therefore, the design of pyrotechnics access is a key link in the safe and reliable design of spacecraft. Whether the design of pyrotechnics is reasonable and whether the verification is sufficient will directly affect the success or failure of the launch mission. [0004] The ...

Claims

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Application Information

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IPC IPC(8): B64G1/44B64G5/00G01R31/00
CPCB64G1/44B64G5/00G01R31/00
Inventor 习成献孔陈杰张强刘恩权何盼陈天明李锐
Owner INNOVATION ACAD FOR MICROSATELLITES OF CAS
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