Project Budget
TL;DR
- Total budget: $200–490 billion (with inflation $250–610 billion over 10 years)
- Import from Earth: ~2,550 t electronics (~100 launches)
Currency and Inflation
All amounts are in 2026 US dollars (USD 2026).
Historical projects are adjusted for inflation. For a 10-year project we account for:
- Average US inflation (2015-2026): ~2.5%/year
- Over 10 years: (1.023)^10 = 1.255 ≈ +25%
- This is a conservative estimate; actual inflation may be higher
| Scenario | 2026 Nominal | With 10-year inflation |
|---|---|---|
| Optimistic | ~$200 billion | ~$250 billion |
| Baseline | ~$355 billion | ~$445 billion |
| Conservative | ~$490 billion | ~$610 billion |
International References (2026)
Launch Costs ($/kg to LEO)
| Country | Vehicle | $/kg | Source |
|---|---|---|---|
| USA | SpaceX Falcon 9 | $2,700-5,000 | Wikipedia |
| China | Long March 5 | $3,000 | China-in-Space |
| China | Long March 8 | $3,550 | NextSpaceflight |
| Russia | Soyuz-2 | $3,800-5,300 | TASS |
| India | PSLV | $8,400-15,000 | SpaceTechAsia |
| Future | Starship, Long March 9, Yenisei | $1,000-1,500 | 2030+ projections |
For calculations: $2,500/kg (mix of current and future technologies)
Rocket Production Costs
| Vehicle | Unit Price | Source |
|---|---|---|
| Starship | ~$100M (estimate) | SpaceX |
| Falcon 9 | ~$50M | SpaceX |
| Long March | $30-50M | CASC |
| Soyuz-2 | ~$35M | Roscosmos |
For calculations: $50M/rocket (international fleet)
AI Development (2026 references)
| Company | Budget/year | Employees | Total spent | Source |
|---|---|---|---|---|
| OpenAI | $7 billion | 1,500 | ~$20+ billion | DCD |
| DeepMind | $12 billion | ~3,000 | ~$50+ billion | Wikipedia |
| Waymo | ~$2 billion | 1,500 | $11 billion over 15 years | VentureBeat |
| Tesla FSD | $10 billion | 800+ | ~$15 billion over 8 years | CleanTechnica |
AI specialist salaries: - OpenAI median: $875K/year - Top researchers: $10-20M/year - International teams (China/Russia): $100-200K/year
Construction in China (references)
| Project | Cost | Area | Source |
|---|---|---|---|
| BYD Shenzhen Phase 2 | $2.87 billion | 3.79 million m² | SCMP |
| Tesla Gigafactory Shanghai | ~$2 billion | 860,000 m² | Public data |
| Average construction cost | ~$580/m² | — | Statista |
Base Calculations (international prices)
1. R&D (excluding AI)
| Item | Estimate | Rationale |
|---|---|---|
| Swarm management software | 1-2 billion | Distributed system |
| VR simulators and training | 0.5-1 billion | |
| Scientific research | 1-2 billion | Materials science, thermodynamics |
| Total R&D | 3-5 billion |
2. AI Development for Robots
Why easier than Waymo/Tesla: - No pedestrians, cyclists, unpredictable people - No traffic rules, signs, intersections — only factory tasks - Fixed operations (mining, assembly) vs infinite driving scenarios - Can fail and retry — not real-time safety-critical
Characteristics: - Autonomy due to 5-20 min communication delay - Extreme conditions require reliable hardware
| Item | Calculation | Estimate |
|---|---|---|
| Team (4,000 people × $150K × 6 years) | ML engineers, roboticists, labelers | 3.6 billion |
| Compute (GPU, data centers) | $0.75 billion/year × 6 years | 4.5 billion |
| Robot prototypes for training | Thousands of units for data collection | 2 billion |
| Data labeling | Labeling millions of scenarios | 1 billion |
| Total AI | 10-12 billion |
Risks: With scaling (more data, complex models) budget may grow to $15-20 billion.
3. Earth Test Site (China)
Why China: - Construction 2-3× cheaper than USA - Faster construction (Tesla Shanghai in 1 year) - Developed industrial base and logistics
Location: Gansu Province — simulating Mercury conditions.
| Item | Calculation | Estimate |
|---|---|---|
| Construction | 2 million m² × $580/m² | 1.2 billion |
| Vacuum chambers | 10 large chambers × $50M | 0.5 billion |
| Thermal-vacuum chambers (-180°C…+430°C) | 0.3 billion | |
| Radiation simulators | 0.2 billion | |
| Factory prototypes | 3-5 full cycle iterations | 2 billion |
| Robot prototypes | Thousands of units, dozens of versions | 1.5 billion |
| Housing and infrastructure | 10,000-15,000 people | 0.5 billion |
| Personnel | 10,000 × $30K × 4 years | 1.2 billion |
| Logistics and materials | 1 billion | |
| Total Earth Test Site | 8-10 billion |
4. Lunar Test Site
| Item | Estimate | Rationale |
|---|---|---|
| Delivery of 60 t to Moon | 4-6 billion | 10-20 launches |
| Test site equipment | 3-5 billion | Factory, robots, concentrators |
| 2 years of operations | 2-4 billion | Management, iterations |
| Total Lunar Test Site | 9-15 billion |
5. Production: Electronics for Self-Replication
Principle: On Mercury, factories and robots are built from local materials (Al, Fe, Si). Only electronics (chips, boards, sensors) are imported from Earth.
| Item | Calculation | Estimate |
|---|---|---|
| Bootstrap factories (E1 × 2) | Full import 280 t | 2.8 billion |
| Electronics for 1649 factories | ~90 t × $3K/kg | 0.27 billion |
| Electronics for 60K robots | ~765 t × $3K/kg | 2.3 billion |
| Electronics for 1000 MDs | ~275 t × $5K/kg | 1.4 billion |
| Chips for 1.1B mirrors | ~1,055 t × $10K/kg | 10.6 billion |
| Vitamins (4 years) | ~509 t × $10K/kg | 5.1 billion |
| Total production | ~2,974 t electronics | ~22.4 billion |
Price justification (international sources 2026):
| Category | Price | Rationale | Sources |
|---|---|---|---|
| Robots, factories | $3K/kg | ARM + LiDAR | 🇬🇧 Raspberry Pi, 🇨🇳 Livox Mid-360 ($2.3K/kg), 🇺🇸 Velodyne ($4.8K/kg) |
| Mass Drivers | $5K/kg | IGBT power electronics | 🇩🇪 Infineon, Semikron, 🇰🇷 SemiHow |
| Mirrors | $10K/kg | Space-grade rad-hard | 🇺🇸 NASA, 🇪🇺 ESA |
| Vitamins | $10K/kg | Iridium ($200K/kg) + rare earths | Strategic Metals, 🇧🇪 Umicore |
Robot references (international):
| Country | Manufacturer | Price | Source |
|---|---|---|---|
| 🇺🇸 USA | Boston Dynamics Spot | $2.3K/kg | IEEE Spectrum |
| 🇨🇳 China | SIASUN, ESTUN | 20-35% cheaper than Western | TAdviser |
| 🇷🇺 Russia | Promobot | <$30K service robot | Promobot |
| 🇮🇳 India | Tata/Mahindra | market +8.8% CAGR | IMARC |
Frames, structures, housings — local production from regolith. Details: Delivery.
6. Rocket Program
| Item | Calculation | Estimate |
|---|---|---|
| Production of ~100 rockets | 100 × $50M | 5 billion |
| Spaceport upgrades | 2-3 billion | |
| Infrastructure | 1-2 billion | |
| Total rockets | 8-10 billion |
7. Launches and Delivery
| Item | Calculation | Estimate |
|---|---|---|
| ~2,550 tons (total) | 2,550 t × $2,500/kg | 6.4 billion |
| Mission control | 11 years of operations | 3-5 billion |
| Total launches | 9-11 billion |
Includes: Moon (80 t) + factories (~370 t) + MD boards (~275 t) + mirrors (1,055 t) + vitamins (765 t). NaS capacitors — local production. See Import Summary.
8. Energy Reception System (Microwave + Rectenna)
Technology: LSP stations on Moon receive Swarm light → PV → 2.45 GHz microwaves → rectenna on Earth.
References (2026): - Caltech SSPP: first space-to-Earth power transmission demo (2023) - JAXA SPS: orbital solar power station program - ESA SOLARIS: space power transmission research - NTT + MHI: 152W transmitted over 1 km via microwaves (world record) - Rectenna efficiency: 85% (current technology)
8.1 Receiver Technology R&D
| Item | Calculation | Estimate |
|---|---|---|
| High-power klystron development | 90% efficiency, scaling | 2-3 billion |
| Rectenna panel development | 2.45 GHz antenna-rectifiers | 1-2 billion |
| Tracking/pointing system | Phased arrays, beam steering | 1-2 billion |
| Earth prototyping | Test site testing | 0.5-1 billion |
| Space demonstration | Pilot Moon→Earth transmission | 0.5-1 billion |
| Total Receiver R&D | 5-9 billion |
8.2 Ground Infrastructure
| Item | Calculation | Estimate |
|---|---|---|
| Rectenna panel production | ~100 stations, GW scale | 8-15 billion |
| Station construction | Site preparation, foundations | 10-20 billion |
| Land rights and approvals | Lease/purchase, frequency regulation | 2-5 billion |
| Environmental reviews | EIA, compensations | 1-3 billion |
| Control system | Tracking, distribution | 1-3 billion |
| Grid integration | HVDC, operator coordination | 3-6 billion |
| Energy storage (buffer) | For night interruptions | 3-6 billion |
| Total ground infrastructure | 28-58 billion |
8.3 Total Reception System
| Subcategory | Minimum | Maximum |
|---|---|---|
| Receiver R&D | 5 | 9 |
| Ground infrastructure | 28 | 58 |
| TOTAL energy reception | 33 | 67 |
9. Additional Items
| Item | Calculation | Estimate |
|---|---|---|
| Communication system (DSN) | Expansion of existing networks | 2-4 billion |
| Propellant production | 450,000 t LOX+methane | 5-8 billion |
| Personnel training | 50,000 people × $50K × 5 years | 12-15 billion |
| International coordination | Lawyers, diplomats | 1-2 billion |
| Mission insurance | 2-4 billion | |
| Total additional | 22-33 billion |
10. LSP Stations on Moon
Instead of an orbital Hub at L1, LSP (Lunar Solar Power) stations on the Moon’s surface are used. Details: Energy Reception Hub.
Why LSP, not Hub?
| Parameter | Orbital Hub (L1) | LSP (Moon) |
|---|---|---|
| Efficiency | 10% | 18% |
| Radiators | 7,900 km² in space | 0 (heat to ground) |
| Mass | 15 million t in orbit | ~178,000 t on surface |
| Resources | Delivery from Moon | In-situ |
LSP Characteristics
| Parameter | Value |
|---|---|
| Stations | 40 on lunar limbs |
| PV area per station | ~160 km² (6,400 km² total) |
| Total mass | ~178,000 t (per data.json HUB-001) |
| Materials | Al 60%, Cu 28%, Si 9%, Fe 0.3% — local |
| Electronics from Earth | ~200-300 t (2-3 launches) |
LSP Cost
| Item | Calculation | Estimate |
|---|---|---|
| Production (ISRU) | Robots and equipment already counted in “Lunar Test Site” | 0 |
| Electronics from Earth | ~250 t × $10,000/kg | 2-3 billion |
| Management and logistics | Construction coordination of 40 stations | 2-4 billion |
| Total LSP | 4-7 billion |
Note: LSP stations are essentially free because production is from lunar materials by robots already counted in other budget items
Summary: Base Estimates
| Category | Minimum | Maximum |
|---|---|---|
| 1. R&D (excluding AI) | 3 | 5 |
| 2. AI Development | 10 | 12 |
| 3. Earth Test Site (China) | 8 | 10 |
| 4. Lunar Test Site | 9 | 15 |
| 5. Production (electronics) | 25 | 32 |
| 6. Rocket program | 4 | 6 |
| 7. Launches | 6 | 8 |
| 8. Energy reception (rectenna) | 25 | 49 |
| 9. LSP stations on Moon | 4 | 7 |
| 10. Additional items | 22 | 33 |
| BASE TOTAL | ~119 | ~183 |
Structure by Location
Grouping by project phases and implementation locations.
Summary (Level 1)
| # | Location | Min | Max | % |
|---|---|---|---|---|
| 1 | Earth (R&D, AI, test site) | 34 | 44 | 24% |
| 2 | Moon (test site + LSP) | 13 | 22 | 11% |
| 3 | Mercury (electronics, rockets, launches) | 38 | 43 | 26% |
| 4 | Energy receiver (rectenna) | 33 | 67 | 32% |
| 5 | Additional items (communications, propellant, training) | 22 | 33 | ~8% |
| TOTAL | ~140 | ~209 | 100% |
Breakdown (Level 2)
1. Earth (~17%)
R&D, AI development, test site, personnel training.
| Subcategory | Calculation | Amount |
|---|---|---|
| R&D (excluding AI) | 3-5 billion | |
| — Swarm management software | Distributed system | 1-2 billion |
| — VR simulators | Operator training | 0.5-1 billion |
| — Scientific research | Materials science, thermodynamics | 1-2 billion |
| AI Development | 10-12 billion | |
| — AI team | 4,000 people × $150K × 6 years | 3.6 billion |
| — Compute | $0.75 billion/year × 6 years | 4.5 billion |
| — Robot prototypes | Thousands of units for training | 2 billion |
| — Data labeling | Millions of scenarios | 1 billion |
| Earth Test Site (China) | 8-10 billion | |
| — Construction | 2 million m² × $580/m² | 1.2 billion |
| — Test equipment | Chambers, simulators | 1 billion |
| — Factory prototypes | 3-5 iterations | 2 billion |
| — Robot prototypes | Dozens of versions | 1.5 billion |
| — Test site personnel | 10,000 × $30K × 4 years | 1.2 billion |
| — Housing and logistics | 1.5 billion | |
| Personnel Training | 13-17 billion | |
| — Staff training | 50,000 people × $50K × 5 years | 12-15 billion |
| — International coordination | Lawyers, diplomats | 1-2 billion |
| Total Earth | 34-44 billion |
2. Moon (~5%)
Technology validation and LSP station construction.
| Subcategory | Calculation | Amount |
|---|---|---|
| Test Site | 9-15 billion | |
| — Delivery of 60 t to Moon | 10-20 launches | 4-6 billion |
| — Test site equipment | Factory, robots, concentrators | 3-5 billion |
| — 2 years of operations | Management, iterations | 2-4 billion |
| LSP Stations | 4-7 billion | |
| — Electronics from Earth | ~250 t × $10,000/kg | 2-3 billion |
| — Management and logistics | 40 stations | 2-4 billion |
| Total Moon | 13-22 billion |
3. Mercury (~30%)
Electronics for self-replication, rocket program, launches.
Self-replication principle: Factories and robots are built on Mercury from local materials. Only electronics (chips, boards, sensors) are imported from Earth — ~2,550 t over 11 years.
| Subcategory | Calculation | Amount |
|---|---|---|
| Electronics (import) | ~21 billion | |
| — Bootstrap factories (E1 × 2) | Full import 280 t | 2.8 billion |
| — Electronics for 1649 factories | ~90 t × $3K/kg | 0.27 billion |
| — Electronics for 60K robots | ~765 t × $3K/kg | 2.3 billion |
| — Electronics for 1000 MDs | ~275 t × $5K/kg | 1.4 billion |
| — Chips for 1.1B mirrors | ~1,055 t × $10K/kg | 10.6 billion |
| — Vitamins (4 years) | ~509 t × $10K/kg | 5.1 billion |
| Rocket Program | 4-6 billion | |
| — Production of ~50-100 rockets | ~75 × $50M | 3.75 billion |
| — Spaceport upgrades | 2 sites | 1-2 billion |
| Launches and Delivery | 6-8 billion | |
| — ~2,550 t to Moon + Mercury | 2,550 t × $2,500/kg | 6.4 billion |
| — Mission control | 4 years of operations | 0-2 billion |
| Total Mercury | ~38-43 billion |
Support (propellant, communications, insurance) — in “Additional Items” section.
4. Energy Receiver (~32%)
Ground infrastructure for energy reception.
| Subcategory | Calculation | Amount |
|---|---|---|
| Receiver R&D | 5-9 billion | |
| — Klystron development | 90% efficiency | 2-3 billion |
| — Rectenna development | 2.45 GHz antenna-rectifiers | 1-2 billion |
| — Pointing system | Phased arrays | 1-2 billion |
| — Prototypes and demos | 1-2 billion | |
| Ground Infrastructure (rectenna) | 28-58 billion | |
| — Rectenna (~100 stations × 100 km²) | 10,000 km² × $0.8-1.5M/km² | 8-15 billion |
| — Station construction | Site preparation, foundations | 10-20 billion |
| — Land rights and approvals | Lease/purchase, frequency regulation | 2-5 billion |
| — Environmental reviews | EIA, compensations | 1-3 billion |
| — Energy storage | Buffers | 3-6 billion |
| — Grid integration | HVDC and coordination | 3-6 billion |
| — Control system | Tracking, distribution | 1-3 billion |
| Total Receiver | 33-67 billion |
Analysis: Which Items Are Underestimated?
Comparison with real projects shows some estimates may be optimistic.
1. AI Development (was: $15-20 billion → revised: $25-40 billion)
References:
| Company | Spent | Result | Source |
|---|---|---|---|
| OpenAI | $20+ billion | GPT-4, no AGI | DCD |
| Waymo | $11 billion over 15 years | No full autonomy | VentureBeat |
| Tesla FSD | $15 billion over 8 years | Level 2 autopilot | CleanTechnica |
| DeepMind | $50+ billion | Research | Wikipedia |
Problem: Helios requires fully autonomous robots in conditions where Waymo/Tesla would fail: - Vacuum, radiation, +430°C/-180°C - 5-20 minute communication delay (no GPS, no real-time) - Unpredictable regolith and conditions
Adjustment for baseline scenario: $18 → $30 billion (+$12 billion)
2. Rocket Program (was: $8-10 billion → revised: $10-14 billion)
References:
| Program | Cost | Result |
|---|---|---|
| SLS | $35 billion | 1 rocket (expendable) |
| Starship | $5-10 billion | Development (no serial production) |
| Long March 9 (planned) | $10-15 billion | Chinese super-heavy |
Thanks to 99.998% localization: Only ~100 rockets needed (not ~54,000). $50M/rocket × 100 = $5 billion — realistic.
If a new rocket is needed (Russia+China): +$5-8 billion for contribution to joint launcher development.
Adjustment for baseline scenario: $55 → $75 billion (+$20 billion)
3. Factory Production (was: $46-49 billion → revised: $60-80 billion)
References:
| Factory | Cost |
|---|---|
| Tesla Gigafactory Shanghai | ~$2 billion |
| Tesla Gigafactory Nevada | ~$5 billion |
| Semiconductor fab (Taiwan) | $12-20 billion |
Counterargument: Helios factories are simple metallurgy, not semiconductors. At 1650-unit series, price drops.
However: These are autonomous space factories on Mercury. $30M/unit at 1650 series — optimistic.
Adjustment: $30M → $50M/factory = $82.5 billion (×1.7)
4. Launches ($55 billion = $2,500/kg) ✓
This estimate is realistic assuming operational 100+ t heavy rockets: - SpaceX Falcon 9: $2,700-5,000/kg (today) - Heavy rockets (target): $1,000-1,500/kg - Long March: $3,000/kg
With developed infrastructure and launcher mix — $2,500/kg is achievable.
Adjustment Summary
| Item | Was (baseline) | Became | Δ |
|---|---|---|---|
| AI Development | 18 | 30 | +12 |
| Rocket program | 9 | 12 | +3 |
| Production | 68 | 100 | +32 |
| Total adjustment | +47 |
This increases the baseline scenario from ~$227 to ~$274 billion, and with ×1.5 reserve — to ~$430 billion.
Three Scenarios (revised)
Optimistic Scenario (~$200 billion)
Conditions: - Heavy rockets operational by 2028, price $1,000/kg - China and Russia take on 50% of production - AI reaches required level in 4-5 years (not 6-7) - Series effect reduces prices by 30% - Self-replication works — only electronics imported
| Category | Estimate ($ billion) |
|---|---|
| R&D (excluding AI) | 3 |
| AI Development | 8 |
| Earth Test Site | 6 |
| Lunar Test Site | 8 |
| Electronics (self-replication) | 25 |
| Rockets | 3 |
| Launches | 5 |
| Energy reception (rectenna) | 25 |
| LSP stations on Moon | 4 |
| Additional | 18 |
| Reserve (+20%) | 21 |
| TOTAL | ~126 billion |
| With ×1.6 margin | ~202 billion |
Baseline Scenario (~$355 billion, or ~$445 billion with inflation)
Conditions: - Launcher mix (Starship + Long March + Soyuz) - International cooperation works - AI requires 6-7 years of development - Moderate delays and overruns - Self-replication works — only electronics imported
| Category | Estimate ($ billion) |
|---|---|
| R&D (excluding AI) | 4 |
| AI Development | 11 |
| Earth Test Site (China) | 9 |
| Lunar Test Site | 12 |
| Electronics (self-replication) | 30 |
| Rockets | 5 |
| Launches | 8 |
| Energy reception (rectenna) | 40 |
| LSP stations on Moon | 5 |
| Additional | 28 |
| Reserve (+30%) | 53 |
| TOTAL (USD 2026) | ~224 billion |
| With ×1.6 margin | ~$358 billion |
| With +25% inflation | ~$448 billion |
Conservative Scenario (~$490 billion, or ~$610 billion with inflation)
Conditions: - Heavy rockets delayed until 2032 - AI requires 8-10 years and additional iterations - Political complications increase costs - Technical problems require rework - Need to develop own super-heavy launcher
| Category | Estimate ($ billion) |
|---|---|
| R&D (excluding AI) | 6 |
| AI Development | 20 |
| Earth Test Site | 14 |
| Lunar Test Site | 20 |
| Electronics (self-replication) | 40 |
| Rockets | 8 |
| Launches | 12 |
| Energy reception (rectenna) | 58 |
| LSP stations on Moon | 7 |
| Additional | 40 |
| Reserve (+50%) | 128 |
| TOTAL (USD 2026) | ~380 billion |
| With ×1.3 margin | ~$494 billion |
| With +25% inflation | ~$617 billion |
Why Not a Trillion?
American projects are inflated due to:
- Cost-plus contracts — contractor benefits from spending more
- Bureaucracy — approvals, reviews, reports
- Contractor monopoly — Boeing, Lockheed without competition
- Legal costs — lawsuits, patents, insurance
Examples of budget inflation:
| Project | Initial budget | Final | Growth |
|---|---|---|---|
| James Webb | $1 billion | $10 billion | ×10 |
| SLS | $9 billion | $23+ billion | ×2.5 |
| F-35 | $233 billion | $400+ billion | ×1.7 |
Why Helios is different:
- International competition — China, Russia, India are cheaper
- Mass production — 1650 factories, 60,000 robots, economies of scale
- Fixed-price contracts — not cost-plus
- Common goal — fewer political games
Comparison with Real Projects
All amounts converted to USD 2026 (with inflation adjustment for historical projects).
| Project | Nominal | USD 2026 | Duration | Result | Source |
|---|---|---|---|---|---|
| Manhattan | $1.9 billion | ~$30 billion | 3 years | Nuclear weapons | Brookings |
| Apollo | $25-28 billion | ~$280 billion | 11 years | 12 people on Moon | Planetary Society |
| GPS (initial) | — | ~$12 billion | ongoing | 31 satellites | Time |
| James Webb | $10 billion | ~$10 billion | 24 years | 1 telescope | Planetary Society |
| SLS (development) | $29-35 billion | ~$35 billion | 13+ years | 1 rocket | Planetary Society |
| ISS | $100-150 billion | ~$150-250 billion | 26 years | 1 station | Wikipedia |
| Tiangong | ~$8 billion | ~$8 billion | ~10 years | 1 station | Estimate |
| Artemis | $93 billion | ~$93 billion (by 2025) | 14+ years | 3 flights | Space.com |
| Three Gorges | ¥200 billion | ~$28-37 billion | 17 years | 22.5 GW | Wikipedia |
| Starship | $5-10 billion | ~$5-10 billion | 10+ years | Rocket | SpaceNews |
| Tesla Gigafactories | $15+ billion | ~$15+ billion | ~10 years | 6 factories | Wikipedia |
| Helios (baseline) | — | ~$355-445 billion | 10-20 years | 10,000 TW | Our estimate |
Conclusion: Helios costs approximately 1.5× Apollo but delivers 4000 times more energy than current planetary consumption. In terms of cost/benefit ratio — the most efficient project in history.
Year-by-Year Distribution (baseline scenario)
| Year | Phase | Main expenses | Amount (billion) |
|---|---|---|---|
| 1-2 | R&D, AI start | AI team, design | 35-45 |
| 3-4 | Earth Test Site, AI | Construction in China, model training | 65-80 |
| 5-6 | Lunar Test Site, production | Lunar missions, mass production | 85-100 |
| 7-10 | Mercury: deployment | First expeditions, Mass Drivers | 80-100 |
| 11-15 | Mercury: scaling | Vitamins, energy reception | 65-80 |
| Total (USD 2026) | 330-405 | ||
| With inflation | ~410-510 |
Known Limitations
Attention: This section describes problems requiring solutions.
High-Priority Issues
1. Testing and Debugging Underestimated
| Stage | Current estimate | Realistic estimate | Rationale |
|---|---|---|---|
| Factory prototypes | 3–5 iterations | 5–10 iterations | 3-5 ground (Gansu) + 2-5 lunar |
| Robot prototypes | $2 billion | $5–10 billion | Hundreds of versions, thousands of units |
| Lunar Test Site | 2 years | 1.5–2.5 years | 3-5 iterations × 3-5 months + deployment |
Reason: The ground test site (Gansu) allows completing major iterations before going to the Moon (TRL 4→6). The Moon validates in the real environment (TRL 6→7-8). Lunar iteration cycle with dedicated launches: ~2-4 months (3-day flight; main time is analysis and fix manufacturing).
Detailed methodology: Risks → Testing Estimation Methodology
Require Research
2. Mission Insurance
- $2–4 billion — optimistic for 10,000 tons of cargo
- At real risk rates, may be 5–10% of cargo value
- Realistic: $5–10 billion for insurance
3. Political Risks
- Sanctions between countries → cooperation breakdown
- Government changes → priority shifts
- Competition instead of cooperation → cost duplication
Cannot be estimated, but potentially +50–100% to budget.
See Also
- Technologies and Sources — TRL and bibliography
- Project in 5 Minutes — what we’re funding
- Roadmap — spending timeline
- Mass Driver — infrastructure and scaling
- Risks — financial risks