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.

Guidelines, Excluding Solar Arrays), 3.2.3 (Internal ESD Design Guidelines), ... Limiting the charge storing material or charging capacity is a useful ... (VDA) metallization on multilayer insulation (MLI) thermal blankets is insufficient to provide adequate shielding for both EMC and internal charging. Layers of aluminum foil mounted to the ...

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  Guidelines, Material, Multilayer, Insulation, Multilayer insulation

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