The invention relates to a dust planet thermal vacuum simulation cabin which comprises a cabin body, a vacuum system, a temperature control system, an illumination simulation system, a dust distribution system and a control system, a sample table is arranged in the cabin body; the vacuum system is used for vacuumizing the interior of the cabin body; the temperature control system is arranged on the cabin body and is used for controlling the temperature in the cabin body; the illumination simulation system is arranged on the cabin body and is used for irradiating the sample table; the dust distribution system is arranged in the cabin body and is used for spraying dust in the cabin body; the vacuum system, the illumination simulation system, the temperature control system and the dust distribution system are all electrically connected with the control system, and the control system is used for controlling the vacuum system, the illumination simulation system, the temperature control system and the dust distribution system to work. The device can continuously run for 21 geophysical days and is closer to the actual environment of a dust planet, so that the test accuracy of a planet surface detection device is effectively improved.
本发明涉及一种尘埃行星热真空模拟舱,包括舱体、真空系统、温度控制系统、光照模拟系统、粉尘分配系统以及控制系统;舱体内部设置有样品台;真空系统用于对舱体的内部进行抽真空;温度控制系统设于舱体上,温度控制系统用于控制舱体内的温度;光照模拟系统设于舱体上,光照模拟系统用于照射样品台;粉尘分配系统设于舱体内,粉尘配系统用于在舱体内喷洒粉尘;真空系统、光照模拟系统、温度控制系统及粉尘分配系统均与控制系统电连接,控制系统用于控制真空系统、光照模拟系统、温度控制系统以及粉尘分配系统工作。本发明能持续运行21个地球日,更接近尘埃行星的实际环境,从而有效提高行星表面探测器件的测试准确性。
Dust planet thermal vacuum simulation cabin
尘埃行星热真空模拟舱
10.03.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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