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High-precision dynamic controllable temperature simulation device

A simulation device, high-precision technology, applied to the simulation device of space navigation conditions, transportation and packaging, space navigation equipment, etc., can solve the problems of rough temperature simulation device, small temperature control range, single temperature control method, etc. Various temperature modes, large temperature control range, and convenient control logic

Active Publication Date: 2020-06-05
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
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AI Technical Summary

Problems solved by technology

In the space environment simulation test, the existing temperature simulation device is relatively rough, usually with a single temperature control method, a small temperature control range, and poor temperature control accuracy

Method used

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  • High-precision dynamic controllable temperature simulation device
  • High-precision dynamic controllable temperature simulation device
  • High-precision dynamic controllable temperature simulation device

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Embodiment Construction

[0023] The application will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain related inventions, rather than to limit the invention. It should also be noted that, for ease of description, only parts related to the invention are shown in the drawings.

[0024] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and embodiments.

[0025] As mentioned in the background technology, in order to verify the influence of temperature environment changes on the performance of the internal sensitive components of the load, it is necessary to provide a controllable temperature change test system in a simulated vacuum low temperature b...

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Abstract

The invention discloses a high-precision dynamically controllable temperature simulation device. The temperature simulation device is used for controlling the temperature of the spacecraft load; the temperature simulation device comprises vacuum cold black environment simulation equipment, a low-temperature platform, a radiation boundary temperature control structure and a conduction boundary temperature control structure. The conduction boundary temperature control structure is arranged on the low-temperature platform; the spacecraft load is arranged on the conduction boundary temperature control structure, the radiation boundary temperature control structure covers the spacecraft load, the radiation boundary temperature control structure and the conduction boundary temperature control structure cooperate to control the temperature of the spacecraft load, the temperature control modes are diversified, the temperature control range is large, and the temperature control precision is high. The radiation boundary temperature control structure and the conduction boundary temperature control structure are not in contact with each other and do not influence each other, so that the control logic is more convenient.

Description

technical field [0001] The invention generally relates to the technical field of spacecraft load ground testing, in particular to a high-precision dynamic controllable temperature simulation device. Background technique [0002] For the temperature-sensitive components of conventional spacecraft loads, in order to ensure its normal use, the requirement for its thermal control system is generally that the temperature fluctuation is not higher than ±0.5°C. [0003] With the continuous deepening of deep space exploration missions, the scientific instruments used as payloads to carry out detection missions are becoming more and more sophisticated. The optical measurement elements, the core components of new space telescopes and space gravitational wave detectors, have put forward ultra-high precision requirements for the temperature environment. [0004] In order to verify the influence of temperature environment changes on the performance of sensitive components inside the load...

Claims

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Application Information

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IPC IPC(8): B64G7/00
CPCB64G7/00B64G2007/005
Inventor 韩潇周盈刘高同邵静怡张磊孙宇肖庆生
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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