I = average current draw during eclipse (A)
t = eclipse duration (h)
DoD = maximum depth of discharge (%)
M = safety margin factor
How do I calculate the battery capacity for an orbital eclipse?
What factors affect the required battery capacity during an eclipse?
Can you explain what an orbital eclipse means for a spacecraft?
How do I convert the calculated amp-hour demand into battery capacity?
What is the importance of accurate battery capacity calculations for spacecraft?
Results are for informational purposes only and do not constitute professional advice.
