Vacuum container used for space target optical characteristic test

A technology of optical characteristics and vacuum containers, applied in the field of space environment simulation, to achieve the effect of ensuring rationality

Active Publication Date: 2019-11-08
BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE
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Problems solved by technology

[0004] Therefore, the present invention proposes a vacuum container for the optical characteristic test of the space target, the purpose is to meet the requirements of the environment and dimensional relationship between the full-scale test ring die and the measurement system, and solve the problem of consistency of the distance between each measurement device and the test target , and all-round observation problems, while meeting the internal heat sink and the suspension requirements of the measurement mechanism, to achieve consistent conditions in all directions in the vacuum environment, and to meet the needs of long-distance testing and convenient operation by personnel

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  • Vacuum container used for space target optical characteristic test
  • Vacuum container used for space target optical characteristic test
  • Vacuum container used for space target optical characteristic test

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Embodiment Construction

[0048]The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.

[0049] Such as figure 1 As shown, the vacuum container provided by the present invention adopts a spherical design, which is the best choice to ensure that the distances from each measuring device to the test target are consistent.

[0050] The present invention is a large-scale spherical vacuum container. From the structural point of view, it is a shape that takes the center of the sphere as the center and equidistantly radiates outward in all directions. Therefore, no matter where the measuring equipment is placed, it can reach the center of the sphere. The distance between the placed objects is the same. In terms of function, the spherical vacuum container is the main structure of the optical simulation test system, and it is the collection center of the heat sink, vacuum system, nitrogen system, measurement and control system and ...

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Abstract

The invention discloses a vacuum container for testing optical properties of a space object, which is characterized in that the main body is a spherical tank, the spherical tank is assembled by spherical shell plates in a partition manner and adopts football slice combination and orange slice combination; the top of the container is connected with a sun simulator, the side surface is provided withan access gate, the container is connected with a transmission light path device, and the container is provided with a plurality functional windows and can realize equidistant measurement of the external radiation measurement. Disclosed by the invention is a large-diameter spherical vacuum container with a diameter of 18m, and the vacuum container can bear the self-weight, the weight of internalheat sinks and the weight of other in-tank measurement and accessory equipment. The container not only satisfies the establishment of the space optical environment, the installation of the measurementequipment and the establishment of a space geometrical relation of full-size test pieces, but also ensures the operation rationality and the structural stability.

Description

technical field [0001] The invention relates to a large-scale vacuum low-temperature ring mold container in the field of space environment simulation, in particular to a vacuum container used for the optical characteristic test of a space object. Background technique [0002] In the optical characteristic simulation test of the space target on the ground, in order to simulate the vacuum and low temperature environment, a large vacuum container is required. In the test, the target needs to be observed from multiple angles, and the angle relationship corresponding to the measurement window should be specially designed, otherwise it will cause measurement errors; and the distance between the measuring equipment and the target should be kept consistent as far as possible, so as to obtain accurate radiation measurement results; And because the test environment requires vacuum, low temperature, and radiation, a lot of auxiliary equipment must be installed inside and outside to ens...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M11/02G01M11/04
CPCG01M11/00
Inventor 孟刚南华薛莲周岩邓蓉李亚男范小礼白文浩王申兆刘鑫刘洪艳刘得成
Owner BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE
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