An Investigation of Low Earth Orbit Internal Charging

[摘要] Built internal charging model for spacecraft design and anomaly assessment that calculates number of internal discharges given material properties and environment characteristics. As shielding decreases, the number of discharges increases. Ungrounded MLI produced a significant number of discharges even through thin layers.

[发布日期] 2014-06-23

[学科分类] 航空航天科学