BRM-loading · layering pigment…
BRM-loading · layering pigment…
Open R&D · space · 5 open problems · substrate contribution paths
Open problems in space-engineering R&D where multi-billion-dollar programs have not yet closed the structural gap. From launch cost floor to crew radiation shielding to Mars sample-return automation, each row names the structural unsolved + substrate contribution path. Average time-to-impact for substrate contributions: 43 months.
cumulative annual R&D spend addressed · USD millions
v1.2026.05.16 · 5 problems · max spend $3,000M · block 946,772
Open-problem ledger · substrate-contribution pathways · Each row names a structurally unsolved R&D problem, the reason the conventional industry has not closed it, and the substrate contribution path the BRMSTE substrate offers. Substrate modes: physics-decomposer · sieve-inference · cross-civilizational-historical-anchor · agentic-routing · three-body-failure-audit. See /legal/liability.
| # | Open problem | Why unsolved | R&D ($M) | Substrate contribution | T-to-impact (mo) |
|---|---|---|---|---|---|
| 01 | Launch cost <$100/kg LEO (engineering pathway) launch-cost-100-leo | reusability cost amortisation · pad turnaround saturating | 3,000 | physics decomposer on structural mass × engine efficiency × logistics residue | 48 |
| 02 | In-situ resource utilisation water extraction · Moon isru-lunar-water | regolith excavation energy-negative · oxygen production margin <5% | 500 | sieve inference on thermal-regolith-interaction + agentic mining-robot control routing | 42 |
| 03 | Crew radiation shielding (active/passive synergy) crew-radiation-shielding | passive material >50 t/crew-habitat · active shielding unproven | 400 | physics decomposer on galactic-cosmic-ray × solar-particle × shielding material trade-off | 54 |
| 04 | Orbital debris remediation at scale orbital-debris-remediation | target tracking + capture dynamics + collision-risk modeling all hard | 200 | agentic tracking + three-body audit (relative motion × capture likelihood × cascade-risk residue) | 30 |
| 05 | Mars in-situ sample-return automation mars-isru-sample-return | contamination control · drilling + sealing + return architecture not integrated | 300 | agentic robotic-sequence planning + cross-civilizational anchor (terrestrial deep-drilling history) | 42 |
“5 open problems in Space · launch · ISRU · habitation. Cumulative annual R&D spend addressed: $4,400M. Each row names the substrate-contribution path. The substrate publishes what it can move; counterparties verify the path before applying.”
Wave OPEN-RD · space · v1.2026.05.16