Vacuum thermal test method of mass production satellite constellation system

A technology of vacuum thermal test and satellite system, which is applied in the field of vacuum thermal test of mass-produced satellite constellation system, can solve the problems that restrict the development progress and launch plan of mass-produced satellites, and achieve shortened development and test cycle, short test cycle, and damage The effect of probability reduction

Active Publication Date: 2019-08-27
上海中科辰新卫星技术有限公司
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Problems solved by technology

[0013] The purpose of the present invention is to provide a vacuum thermal test method for mass-produced satellite constellation system to solve the problem

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  • Vacuum thermal test method of mass production satellite constellation system
  • Vacuum thermal test method of mass production satellite constellation system
  • Vacuum thermal test method of mass production satellite constellation system

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[0070] In the following, the satellite system vacuum thermal test method proposed by the present invention will be further described in detail with reference to the accompanying drawings and specific embodiments. According to the following description and claims, the advantages and features of the present invention will be clearer. It should be noted that the drawings are in a very simplified form and all use imprecise proportions, which are only used to conveniently and clearly assist in explaining the purpose of the embodiments of the present invention.

[0071] The core idea of ​​the present invention is to provide a mass production satellite constellation system vacuum thermal test method to solve the problem that the existing mass production satellite constellation test method seriously restricts the development progress and launch plan of the mass production satellite.

[0072] In order to realize the above ideas, the present invention provides a mass production satellite con...

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Abstract

The invention provides a vacuum thermal test method of a mass production satellite constellation system. A plurality of satellites are put into space environment simulation equipment simultaneously, thermal balance satellites and thermal vacuum satellites are selected correspondingly, and thermal control states of the thermal balance satellites are worse than that of the thermal vacuum satellites;a thermal balance test is carried out on the thermal balance satellites; during the process of the thermal balance test, equipments on the thermal balance satellite is powered up according to an in-orbit established working mode, and external thermal flow is applied to the surfaces of the thermal balance satellites according to external thermal flow design parameters; the external thermal flow ofthe thermal balance satellites is corrected in real time by simulating the influence of the mutual occlusion of the satellites on the external thermal flow of the thermal balance satellites; and during the process of the thermal balance test, the equipment on the thermal vacuum satellites is powered up according to an in-obit established working mode, and no external thermal flow is applied. After the thermal balance test is completed, the high and low temperature range of a thermal vacuum test of the satellite system is determined according to thermal balance test results, and the thermal vacuum test of the tested satellite system is carried out.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a vacuum heat test method for batch production of satellite constellation systems. Background technique [0002] With the continuous development of aerospace technology, the functional density of spacecraft is getting higher and higher. At present, the miniaturization and batch development and production capacity of spacecraft have been realized. A satellite constellation is a collection of several or more satellites that are launched into orbit and can work normally, have similar functions, and are combined in a certain way. For the completion of tasks such as global communication, navigation and environmental monitoring, any place on the earth must be covered by satellites at any time. To achieve this, it is not enough to use one satellite, and multiple satellites are needed in a certain way. Form a satellite network to realize the above functions. At this stage, miniaturi...

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Application Information

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IPC IPC(8): B64G7/00B64G99/00
CPCB64G7/00B64G2007/005B64G99/00
Inventor 林士峰林宝军蒋桂忠沈苑王国际张军李锴马二瑞
Owner 上海中科辰新卫星技术有限公司
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