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Chapter 3 Spacecraft Design Guidelines - NASA

31 Chapter 3 Spacecraft Design Guidelines Section describes processes involved in immunizing a Spacecraft against Spacecraft charging problems. Section lists Design Guidelines . If the reader wishes to make a requirements document, the basic requirements include: a. Determine whether or not the mission passes through or stays in regions with a charging threat. b. If in a charging threat region, determine the threat that is applicable to that environment. c. Implement measures to mitigate the threat to an acceptable level.

electronic components to optical parts. (Discharging in glass has long been . Spacecraft Design Guidelines 33 known to cause fracturing and damage to optical windows or dielectrics, but ... material properties needed are the ability to accumulate charge, i.e., resistivity or conductivity, and the pulse threat, e.g., stored voltage, energy ...

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