Transcription of Chapter 3 Spacecraft Design Guidelines - NASA
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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. Sections (General ESD Design Guidelines ), (Surface ESD Design Guidelines , Excluding Solar Arrays), (Internal ESD Design Guidelines ), (Solar Array ESD Design Guidelines ), and (Special Situations ESD Design Guidelines ) can be used as aids.
orbits and today’s hardware, an adequate shielding level has been on the order of 110 mil of aluminum-equivalent shielding, but 200 mil is more conservative and may be necessary for certain situations (Section 3.2.3.2.2). For some ESD-immune hardware, the amount needed may be less; it almost certainly will
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