Not everything here is finished. That is the point.
A regenerative CO₂ preprocessor for lunar habitats. Started mid-March 2026 after an email from Space Center Houston. Built by an 8th grader.
661 pounds. 600 watts.
Vents CO₂ into space.
Does not work on the Moon — no 'into space.'
Single-use. 1,440 needed for 180 days.
Over 6,000 pounds of dead mass.
The math does not close.
Regenerative. 0.99 lb. ~8W.
Captures, releases, repeats.
No canisters. No vents. Just zeolite and heat.
Silica gel strips moisture from cabin air. Humidity kills CO₂ capture efficiency, so this happens first.
Zeolite 13X bed captures CO₂ at room temperature. Nitrogen and oxygen pass through. Clean air returns to the cabin.
Heat to 248°F. CO₂ desorbs from zeolite as concentrated gas. Chamber is sealed — cabin loop stays isolated.
Sweep gas pushes concentrated CO₂ through compressor into buffer tank at 22 psi. Steady feed for the Sabatier reactor.
AERO-LITE Phase 1 prototype — three mason jars with zeolite beads, silica gel, and CO₂ sensors on a desk
This is not a rendering. It is three mason jars on my desk, a live ESP32-S3, and a web dashboard that updates every second.
Live data: Cabin 1,029 ppm → Purified 477 ppm. Capture visible in real time.
My first design compressed cabin air directly. The math showed 99% of that energy compresses nitrogen, not CO₂. I felt stupid. Then I fixed it. That is engineering.
Pressure swing uses less energy, but vacuum seals in microgravity are catastrophic leak risks. A PTC heater with a bimetallic cutoff is safer — even if the ESP32 crashes.
Judges see 50 slide decks. They remember the one with a photo of real hardware and a URL where they can watch numbers change. Proof beats promises.
All firmware, schematics, 3D models, and documentation are open source.