Question: 4. Given a single Li-Ion battery and 0.85 transmission efficiency, calculate the required capacity of the battery. A spacecraft in a circular, equatorial orbit has

4. Given a single Li-Ion battery and 0.85 transmission efficiency, calculate the required capacity of the battery. A spacecraft in a circular, equatorial orbit has flat solar panels the following properties, Pe = Pd = 1150 W Xd = 0.81 a = 6828 km Xe =0.57.

In homework 1, question 4, what approximate depth of discharge should be used for the number of cycles required? 60+% 40% 13% 24%

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