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Extra resources for Practical Considerations in Applying Electronics to Space Systems
Reasons most of the external surfaces are electrical insulators. When bombarded with ionized particle radiation, an electrical charge can result. Since the particles have high energies, the charge increases until there is a voltage breakdown, and an electrostatic discharge. These discharges produce electrical currents that can induce currents in nearby electrical wires. These in turn can trigger various events in a satellite, and modify stored data. These events have been known for many years, and have been studied under laboratory conditions.
The current is now in the opposite direction to the voltage, that is, producing power. The maximum power is generated when the product of the current and is a maximum; this is labeled the maximum power point. voltage When the voltage changes from the maximum power voltage the power sometimes by a significant amount. D. igure 21 A simple I Connections equation IL = 10 = q. 3 Solar = strings the of current IL - 10(eW/akT solar I of - cells. 38 x 10-23 J/K) absolute temperature adjustable constant of the order of unity While not exact, with temperature, temperature of for I where 1 this so dependence.
R. D. Gordcm recent textbook (Gordon of the figures are from it. Most of also in the author’s handbook (Morgan and Gordon, on the geostationary orbit is in Pocha, 1987. Bazovsky (1961) is easy to read, and emphasizes COMSAT (1975), Solar and Practice, Principles A. M. Nakamura, F. VI On-board SS-TDMA Tech. I-56 Rev. ” COMSAT 21 T. Prentice- of CommunicaAssal, Subsystem (l), 191-225. and B. 6 1 260 I 8 240 I 280 Spacecraft mass, kg(wlthout Figure 52 Reliability versus the communications excluding Morgan, W.