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A kind of pyrotechnics detonation control system and test method thereof

A technology of a control system and a test method, which is applied in the aerospace field, can solve problems such as difficult measurement, limited test safety of the explosive detonation control system, insufficient test site, and inadequate testing of explosive devices, so as to improve work efficiency, The effect of improving reliability and safety

Active Publication Date: 2022-03-15
INNOVATION ACAD FOR MICROSATELLITES OF CAS +1
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  • 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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  • A kind of pyrotechnics detonation control system and test method thereof
  • A kind of pyrotechnics detonation control system and test method thereof
  • A kind of pyrotechnics detonation control system 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 an explosive detonation control system, which realizes the control of the explosive initiation through three-level control. The control system includes a control circuit and a protection and measurement system, wherein the control circuit includes a first relay, a second relay, and a third relay for controlling the on-off of the circuit, a current-limiting resistor connected in series with the relay, and a case ground for leakage. The discharge resistor for discharging static electricity; and the protection and measurement system includes multiple star meter sockets. By inserting the protection plug or the launch plug in the star meter socket, the on-off of the pyrotechnics control circuit can be controlled, and it can be used multiple times at any stage. Measure the detonation circuit, detonation sequence and bridge wire resistance of pyrotechnics.

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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Patent Type & Authority Patents(China)
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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