This invention discloses a space-simulated
environment variable-temperature photothermal performance testing device based on steady-state
calorimetry: the outer layer of the experimental chamber is a
vacuum chamber, and the inner layer is a cryogenic chamber, with gas communication between the
vacuum chamber and the cryogenic chamber; before testing, the cryogenic chamber is cooled by a cooling device, and the interior of the experimental chamber is evacuated to a
vacuum state by a suction device, so that the interior of the experimental chamber meets the testing environment. A sample installation and adjustment unit is used to install and fix the sample to be tested in the cryogenic chamber. A
temperature control unit is used to change the temperature of the sample to be tested. A solar
radiation simulation unit is used to simulate
sunlight irradiation. When the sample to be tested reaches the preset temperature, the
data processing unit records the corresponding
vacuum level and the output power of the
temperature control unit, and calculates the
emissivity of the sample to be tested by combining parameters such as the temperature inside the cryogenic chamber and the radiative area of the sample. This invention achieves continuous and simultaneous measurement of full-spectrum hemispherical
infrared emissivity and
solar absorptivity from 150K to 450K, with a large temperature range and high measurement accuracy.