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.
(MLI) thermal blankets is insufficient to provide adequate shielding for both EMC and internal charging. Layers of aluminum foil mounted to the interior surface and properly grounded can be used to increase the shielding effectiveness of blankets or …
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