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Microgravity experimental system for component performance verification of plate type propellant management device

A technology of plate propellant and test system, applied in the field of microgravity test, can solve problems such as impossible to obtain from foreign literature, no mention of test system design, incomplete data, etc., achieving high test efficiency and economic benefits, wide Application value and promotion prospects, simple and compact structure

Active Publication Date: 2015-07-08
BEIJING INST OF CONTROL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] At the same time, since the development of plate-type PMD propellant storage tanks and related test verification technologies involve national security, countries that have mastered this technology often impose technical blockades. The information that can be provided by foreign countries is not comprehensive and can only serve as a reference. None of the relevant articles mentioned the detailed test system design. The mechanism research of the plate tank must build a test system by itself to carry out a large number of microgravity tests and obtain sufficient first-hand information. It is impossible for these basic information to be obtained from obtained from foreign literature
[0004] In summary, a microgravity test system for performance verification of plate-type PMD components is the result of exploration and summary during the development of large-capacity plate-type PMD propellant tanks. The entire test system is brand new, and there are no relevant documents and materials in China. It can be used as a reference, and foreign countries rarely disclose similar test systems

Method used

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  • Microgravity experimental system for component performance verification of plate type propellant management device
  • Microgravity experimental system for component performance verification of plate type propellant management device

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Embodiment Construction

[0018] Such as figure 1 As shown, the present invention includes a test system substrate 1, a height-adjustable test bracket assembly, an image acquisition system, a lighting system, and other parts, and the height-adjustable test bracket assembly, image acquisition system, and lighting system are all on the test system substrate 1 Two sets are arranged symmetrically, and the test system has the ability to conduct microgravity tests of two test models at the same time.

[0019] The test system substrate 1 is a light circular aluminum plate with a wood honeycomb layer inside, which is used to realize the compact installation and fixing of the height-adjustable test bracket components, image acquisition system, lighting system, etc., and realize the test system and microgravity at the same time The test cabin is installed and connected.

[0020] The height-adjustable test support assembly is made up of two support plates and two supports, and the first support plate 3 and the s...

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Abstract

A microgravity experimental system for the component performance verification of a plate type propellant management device comprises an experimental system baseplate, height adjustable experimental support assemblies, image collecting systems, illuminating systems, and the like, and is provided with two experimental models simultaneously, namely, two sets of the height adjustable experimental support assemblies, the image collecting systems, the illuminating systems and the like are all arranged on the experimental system baseplate symmetrically. The experimental system has the advantages that the structure is simple and compact, the efficiency is high, the adjustability is strong, the replacement of the models is easy, the image collection is convenient, the system can be realized easily and the like. According to the invention, a microgravity experiment of experimental models of plate type PMD components can be performed, the fluid transmission characteristic and the fluid management capability of all the plate type PMD component models can be obtained, and the PMD performance can be subjected to verification.

Description

technical field [0001] The invention relates to the technical field of test and verification of fluid transmission performance and management performance of a plate-type propellant management device (PMD) under microgravity conditions, and can be popularized and applied to microgravity tests of scaled models of various plate-type PMD components. Background technique [0002] With the rapid development of large-scale truss platform satellites in the world, propellant tanks using plate PMDs have become the mainstream in the world. Since the end of the "Eleventh Five-Year Plan", the development of large-capacity plate-type PMD propellant storage tanks has been carried out. The plate-type PMD prototype has been developed, and the ground demonstration test of the plate-type PMD fluid transmission performance and management performance has been carried out. This demonstration test can only verify the local performance of the plate-type PMD, and cannot truly reflect its ability to ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G7/00
Inventor 胡齐李永潘海林陈健魏延明李泽
Owner BEIJING INST OF CONTROL ENG
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