Comprehensive environment heat balance test system for Mars probe single-machine product

A Mars probe and comprehensive environment technology, which is applied in the testing of machine/structural components, instruments, measuring devices, etc., can solve the problems such as the inability to accurately simulate the absorption ratio of the outer surface state of the product, and the lack of collimation of the infrared heating device. Achieve ease of design and implementation, improved work reliability, and ease of control

Inactive Publication Date: 2020-07-28
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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Problems solved by technology

However, for the simulation of the solar radiation of Mars rover products on the surface of Mars, infrared heating devices are mostly used for simulation. Compared with solar radiation, infrared heating devices are not collimated, and the energy distribution of the spectrum is similar to solar radiation It is very different and cannot accurately simulate the absorption ratio of the outer surface state of the product to solar radiation

Method used

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  • Comprehensive environment heat balance test system for Mars probe single-machine product
  • Comprehensive environment heat balance test system for Mars probe single-machine product
  • Comprehensive environment heat balance test system for Mars probe single-machine product

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Embodiment Construction

[0056] The comprehensive environmental heat balance test system for Mars rover stand-alone products of the present invention will be described in detail below in conjunction with the accompanying drawings. The specific implementation is only for the purpose of illustration and is not intended to limit the protection scope of the present invention.

[0057] refer to Figure 1-3 , Figure 1-3 Respectively show the outline view of the comprehensive environmental heat balance test system for the Mars probe stand-alone product of the present invention, the structure top view in the container of the comprehensive environment heat balance test system for the Mars probe stand-alone product of the present invention (display Mars surface wind The internal structure of the simulation system), the structure side view in the container of the comprehensive environmental heat balance test system for the Mars probe stand-alone product of the present invention (showing the external outline of ...

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Abstract

The invention discloses a comprehensive environment heat balance test system for a Mars detector single-machine product. The system comprises a Mars environment simulation chamber, a solar irradiationsimulation system, a Mars atmosphere simulation system, a Mars surface wind simulation system, a temperature control system and a test piece support system, wherein the Mars environment simulation chamber is a horizontal and capsule-shaped cabin body, container gates which can be opened are arranged at the two ends of the cabin body, and the Mars environment simulation chamber is mainly used forforming a closed space without obvious leakage and maintaining a special atmospheric environment in the cabin. The system can provide comprehensive stress environment tests of five parameters including gas atmosphere, wind speed, pressure, solar irradiation and environment temperature on the surface of Mars, and is easy to operate and good in generalizability.

Description

technical field [0001] The invention belongs to the technical field of spacecraft ground environment simulation test equipment. Specifically, the invention relates to a five-integrated ground comprehensive test equipment that can simultaneously simulate the gas atmosphere, wind speed, pressure, solar irradiation and temperature environment on the surface of Mars. The invention is aimed at the field of heat balance test of Mars environment, but can be extended and applied to test simulation of stratosphere and other environmental factors including solar radiation, temperature, low pressure, wind field and the like. Background technique [0002] At present, Mars exploration has become an important goal of deep space exploration in my country's aerospace industry, and the difference between Mars exploration and other deep space exploration missions lies in the special thermal environment on the surface of Mars. In the Martian surface environment, the main factors affecting the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M99/00B64G7/00
CPCB64G7/00G01M99/002G01M99/005
Inventor 刘守文叶田园周原王浩闫琦郭佳诚陈安然刘旭升靳海洋丁磊
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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