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Calculate the approximate Debye shielding length (in mm) of a spacecraft in a 300 km orbit under the following conditions: 3.1) Night, minimum solar
Calculate the approximate Debye shielding length (in mm) of a spacecraft in a 300 km orbit under the following conditions: 3.1) Night, minimum solar cycle 3.2) Day, maximum solar cycle Assume that the same plasma temperature as for question 2.
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