Abstract

ABSTRACT (NASA‑Facing)

NASA’s Moon and Mars missions face four persistent engineering challenges:

  1. Corrosive brine handling (Mars ISRU water extraction)

  2. Thermal management in vacuum (habitats, rovers, ISRU plants)

  3. Dust‑resilient fluidics (regolith destroys seals and bearings)

  4. Low‑maintenance, solid‑state systems (long-duration missions)

This disclosure presents NMUS‑1.0, a unified, solid‑state, open‑hardware upgrade suite integrating four builder‑ready Caldwell inventions from the TDC ecosystem:

  • The Nexus Cell — Arachne Gyroid Structural‑Thermal Substrate

  • Arachne Gen‑3 v3.4.1 “FORTRESS” — High‑Thermal Dyneema Microfluidic Interposer

  • Thermal‑Energy Harvesting Loop (TEHL‑v1.0) — Vacuum‑Compatible Waste‑Heat Recovery

  • TV‑RPPH V3.0 — Mars‑Optimized Solid‑State MHD Brine Pump

All components are grounded in standard physics and use materials and fabrication methods available to NASA and commercial aerospace partners.

This architecture is ready for prototype fabrication and testing immediately.

Creative Commons License

Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 License.

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