Ground simulation test method of a spatial comprehensive environment effect of polymeric material used for spacecraft
A technology that aggregates materials and integrates the environment. It is used in material analysis using radiation, material analysis using wave/particle radiation, and material analysis. It can solve problems such as lack, and achieve the effect of simple steps, wide application prospects, and easy operation.
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specific Embodiment approach 1
[0020] Specific implementation mode one: refer to Figure 1 to Figure 4 This embodiment is described in detail. A ground simulation test method for space comprehensive environmental effects of polymer materials for spacecraft described in this embodiment, the method includes:
[0021] Step 1. Place the temperature control device and the temperature control sample stage in the sealed cavity, the temperature control device is used to control the temperature of the temperature control sample stage, and the leads of the temperature control device are connected by the vacuum plug in the sealed cavity;
[0022] Step 2, preparing a test sample of the polymeric material to be tested with a thickness t, testing the initial performance parameters of the sample, and then placing the sample on a temperature-controlled sample stage;
[0023] Step 3. For the test sample in step 2, select the energy of incident electrons, incident protons and incident heavy ions, wherein the incident depth o...
Embodiment
[0030] The test sample is selected as a Teflon material with a thickness of 100 μm and an area of 1 cm×3 cm. The test condition is under vacuum condition, the vacuum degree is 10 -3 Pa. figure 2 The experimental results of the effects of vacuum and thermal cycles on the properties of Teflon materials under different doses of electron irradiation are given. In the figure, the thermal cycle conditions are: temperature range is -100°C to +50°C, the number of cycles is 200, and the heating and cooling rate is 5°C / min; the irradiation conditions are: electron energy 150keV, electron radiation flux 1e10e / cm 2 s. The irradiation area is 4cm×4cm, the irradiation unevenness is less than 5%, and the incident angle of electrons is perpendicular to the sample surface. Depend on figure 2 It can be seen that the degree of damage to the polymer material is greater when vacuum, thermal cycling, and irradiation exist simultaneously.
[0031] image 3The effects of different thermal cy...
specific Embodiment approach 2
[0033] Specific implementation mode two: this implementation mode is to further explain the ground simulation test method for space comprehensive environmental effects of polymer materials for spacecraft described in specific implementation mode one. In this embodiment mode, in step three, protons, heavy The irradiated area of the test sample by ions and electrons should be at least 1.5 times the area of the test sample.
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