







I applied standard utility-scale solar PV design workflows to the lunar surface
With the Artemis II launch, I decided to stress-test our solar engineering tools against a very non-standard environment - the Moon.
I work in utility-scale solar. Our typical workflow: terrain modeling → irradiance analysis → racking/layout design → energy yield simulation. We applied the exact same pipeline to two lunar sites.
Site A - Equatorial (Mare Tranquillitatis)
- ~14.5-day solar cycle (day/night)
- GHI equivalent during lunar day is extreme - no atmosphere, no diffuse component
- Flat terrain, minimal grading challenges
- Critical problem: 354 hours of continuous darkness per cycle - storage requirements would be massive
Site B - Polar (Shackleton Crater Rim)
- Low solar elevation angle (~1.5°–6°)
- Peaks of eternal light with up to ~90% annual illumination
- Complex topography - steep gradients, shadowing from crater rim features
- Near-continuous generation but at significantly reduced intensity
Key engineering observations
- The atmosphere-free environment eliminates diffuse irradiance entirely - every photon is direct (DNI = GHI)
- Racking design differs radically: equator uses near-flat tilt, pole needs near-vertical panels to catch low-angle sun
- The energy yield delta between sites is ~2.5x - the continuous generation at the pole wins over peak-but-intermittent equatorial output
Full modeling results in the images. Curious to hear from other engineers - what assumptions would you challenge?







