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Power & Energy Budget

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Size a spacecraft solar array and battery from orbital energy balance, eclipse load, storage limits, and explicit power margins.

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Required array power

310.2 W

263.7 W after degradation

Battery capacity

129.6 Wh

77.8 Wh bus energy

Orbit energy

190.0 Wh

70.0 Wh during eclipse

Peak ratio

0.68

peak load / EOL array

Orbit power balance

Solar generation must carry sunlit loads and replace battery energy before the next eclipse.

60 min sun / 35 min eclipse

Suneclipse shadowsunlighteclipse

End-of-life array

263.7 W

310.2 W beginning-of-life before degradation

Battery at bus

77.8 Wh

60% depth of discharge drives installed capacity

Total orbit load

190.0 Wh

90% distribution efficiency, 90% battery round trip

Open Source and Easy to Use Elsewhere

This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.

Open source: review the implementation and see how the results are produced.

Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.