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Polar orbit satellite bus power cable secondary discharge ground simulation test system and method

A secondary discharge and power cable technology, applied in the field of measurement, can solve the problems of insufficient depth, lack of protection methods and design methods, and achieve the effect of improving effectiveness and accuracy

Active Publication Date: 2014-04-30
LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, our country's understanding of the secondary discharge of the busbar power cable of high-power satellite high-voltage solar cells is not deep enough, and there is a lack of effective protection methods and design methods.

Method used

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  • Polar orbit satellite bus power cable secondary discharge ground simulation test system and method
  • Polar orbit satellite bus power cable secondary discharge ground simulation test system and method
  • Polar orbit satellite bus power cable secondary discharge ground simulation test system and method

Examples

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Embodiment 1

[0028] refer to figure 1 , is a schematic diagram of a ground simulation test system for secondary discharge of a polar-orbiting satellite bus power cable in an embodiment of the present invention. In this embodiment, the ground simulation test system for a secondary discharge of a polar-orbiting satellite bus power cable may include: The camera 1 of the secondary discharge phenomenon, the electron gun 2 for simulating the aurora electronic environment of the polar-orbiting satellite, the target chamber 3, the vacuum pumping system 4 for evacuating the target chamber, including multi-layer insulating film 8 bundled wires 9 and cables 10 to simulate the test sample 5, sample support 6 and test circuit 7 of the polar-orbit satellite bus power cable; the test circuit 7 includes: a voltage source 18 for inducing the secondary discharge of the cable , and a power supply 10 for applying current to the beamline to generate heat to simulate the space thermal environment of a polar-orb...

Embodiment 2

[0036] refer to image 3 , is a flow chart of a ground simulation test method for secondary discharge of a polar-orbiting satellite bus power cable in an embodiment of the present invention. This embodiment can adopt any of the polar-orbiting satellite bus power cable secondary discharge ground simulation tests described in Embodiment 1 system. In this embodiment, the ground simulation test method for secondary discharge of the power supply cable of the polar-orbit satellite bus can specifically include the following steps:

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Abstract

The invention provides a polar orbit satellite bus power cable secondary discharge ground simulation test system and method. The polar orbit satellite bus power cable secondary discharge ground simulation test system comprises an electronic gun, a target chamber, a vacuum pumping system, test samples, a sample support, a test circuit and a camera. The electronic gun is used for simulating the polar light electronic environment of a polar orbit satellite, the test samples comprise bunches and cables wrapped by a plurality of insulating films so as to simulate a polar orbit satellite bus power cable, the test circuit comprises a voltage source and a power source, the voltage source is used for inducing the cable to conduct secondary discharge, and the bunches are powered by the power source. In the target chamber, the camera and the electronic gun are mounted on the top of the target chamber, the sample support is mounted on the bottom face of the target chamber, and the test samples are placed on the sample support. On the outer portion of the target chamber, the test circuit is connected with the test samples, and the vacuum pumping system is connected with the target chamber. According to the system and method, effectiveness and accuracy of the polar orbit satellite bus power cable secondary discharge ground simulation test are improved.

Description

technical field [0001] The invention relates to the field of measurement technology, in particular to a ground simulation test system and method for secondary discharge of a polar-orbit satellite bus power cable. Background technique [0002] The instantaneous orbit plane where the polar orbiting satellite is located and the sun always maintain a fixed orientation, which can make the time of the place where the satellite passes by basically the same, and the satellite remote sensing detection data has long-term comparability. Because the inclination angle of this kind of satellite orbit is close to 90°, the satellite almost passes through the poles, so it is called "near polar sun synchronous orbit satellite", or polar orbit satellite for short. [0003] The safety and reliability of the satellite energy system is related to the function and life of the satellite. With the continuous emergence of new technologies and new demands for satellites, the requirements for the satel...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R31/00
Inventor 王俊李得天杨生胜秦晓刚陈益峰史亮汤道坦柳青赵呈选
Owner LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
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