Determination of threshold values of parameters of electronic irradiation of glass leading to electrostatic discharges

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Experimental data are presented on the minimum values of energies and flux densities of electrons, the impact of which on the cover glasses of solar batteries and reflecting elements of thermoradiators of artificial Earth satellites leads to electrostatic discharges. It has been established that the addition of protons to the composition of the particle flux acting on the studied samples can suppress the development of discharges. For a qualitative interpretation of the results obtained, a mathematical model is proposed.

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作者简介

R. Khasanshin

JSC “Kompozit”; Bauman Moscow State Technical University

编辑信件的主要联系方式.
Email: rhkhas@mail.ru
俄罗斯联邦, Korolev, 141070; Moscow, 105005

D. Ouvarov

JSC “Kompozit”

Email: rhkhas@mail.ru
俄罗斯联邦, Korolev, 141070

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2. Fig. 1. 2D images of 5×5 μm2 fragments of the surface of the original (a) and irradiated sample (c) and their sections along the line 1–1’, 2–2’ (b) and 3–3’ (d), respectively.

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3. Fig. 2. Oscillograms of currents characteristic of the processes accompanying electron irradiation of PS and OE samples (a and b) and OE (c–e): a – type 1 discharges at Ee0 = 15 keV (1), 30 keV (2), 45 keV (3); b – type 1 discharge initiates a similar discharge on the adjacent surface area; c – breakdown on the metal substrate; d and e – respectively, breakdown on the metal substrate initiates type 1 discharge and vice versa; e – breakdown initiates type 2 discharge.

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4. Fig. 3. Dependence of the number of discharges per minute on the electron flux density for different values ​​of Ee0.

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5. Fig. 4. Schematic diagram of the computational domain: ГP – electron gun-vacuum boundary; V – vacuum; G – glass; D – dielectric; ГV–G – vacuum-glass boundary; ГG–D – glass-dielectric boundary; and – electron velocities upon exiting the electron gun and upon entering the glass, respectively; ΩV and ΩG – regions of the problem solution in vacuum and glass, respectively.

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6. Fig. 5. Dependence of the electron energy upon entering the target on the irradiation time (a) and the distribution of the concentration of electrons injected into the PS at different moments of irradiation time (b): 0.1 s (1); 10 s (2); 20 s (3).

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7. Fig. 6. Distribution of electron flux density over the irradiated surface of the PS at different moments of irradiation time: 0.1 s (a); 10 s (b); 20 s (c).

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