How much StarRoad costs
Costs and payback
Capital expenditure, financing structure, launch cost and sources of payback.
~$300 billionmedian estimate for the complete system
$100–150 billionGATES and storage
$150–200 billiontransport component
8–12 yearscombined payback estimate
Economic model
Capital costs, the energy component, storage systems, industrial centres, launch cost and payback dynamics.
Methodology and key assumptions
The economic model is based on the following principles:
- Serial and self-production reduction in equipment costs (PCTs, generators, storage units) by 30–50% due to scale.
- Localisation—the use of African resources, labour and construction materials, supported by Spon’s African Construction Cost Handbook.
- Account of current market prices for energy storage systems (BESS) and geothermal stations according to data for 2025–2026 years.
- Currency rates 1 USD ≈ 100 RUB / 0.90 EUR (for context). All calculations in US dollars 2025 The inflation rate is not the same as the year before. ±30% is in line with the standards of the preliminary TEE.
Tunnel-boring costs under African conditions
- Spon's African Construction Cost Handbook provides detailed data on construction costs in 13 African countries, including labor and material rates. There are no direct proportional figures for large diameter tunnels in the source due to the high variability of conditions, but it serves as a basis for calibrating estimates.
| Type of work | Quantity | Average cost per km | Total cost (USD billions) | Basis |
|---|---|---|---|---|
| The main tunnel (17.5×12.5 m) | 2050 km | $12–18m | $24.6–36.9 | Extrapolated from international data for large cross-sections with adjustment for African conditions. |
| Collector's (6×2050 km, ø2 m) | 12 300 km | $3–5m | $36.9–61.5 | Based on actual data from mining operations in Africa ($3,500/m for small sections). |
| Service tunnel (ø3 m) | 2050 km | $4–6m | $8.2–12.3 | Similar to collector tunnels, adjusted for the larger cross-section. |
| The slopes (40×16 km, 17.5×12.5 m) | 640 km | $12–22m | $7.7–14.1 | Similar to the main, with an addition for the angle of inclination 30°. |
| Total tunnelling | 17 040 km | $77.4–124.8 |
Tunnel-boring machine fleet with in-house production
- When ordering in series (40 the main + 240 service collector + 40 TPPs) and organizing their own assembly line (Gabon and DR Congo) the costs are reduced by 30–50%.
| Machine type | Diameter | Quantity | For 1 pieces (series, own production) | Total (USD billions) |
|---|---|---|---|---|
| Main TBM (SR-Main) | ~18 m | 40 It is. | $35–60m | $1.4–2.4 |
| Collector TBMs (SR-Collector) | 2 m | 240 It is. | $0.8–1.5m | $0.19–0.36 |
| Service TBM (SR-Service) | 3 m | 40 It is. | $1.2–2m | $0.05–0.08 |
| The assembly plants (2 pieces) | — | — | $1–2 billion | $1–2 |
| Total TBM fleet | $2.64–4.84 |
Geothermal Autonomous Thermal Energy System (GATES)
- Real geothermal station with capacity 35 The MW in Kenya (Menengai) is down to ~$35–40 That's a million dollars, which is a lot of money.1,000–1,250/kW (with the drilling and steam wells in mind). When building in series 40 The cost of the station and the localization of production can be estimated at $800–1,200- It's a kilowatt.
- The cost of one station 2.5 GW: $2.0–3.0 billion.
- Cost of 40 stations: $80–120 billion.
- This assessment is confirmed by the lower limit of costs for Russian GeoTES (according to ITURUP about $650/kWt) and the upper limit for complex projects ($1,500/kWt).
- The calculation is based on the upper estimate of the total power of the GATES in 100 GW. The actual available power can only be estimated after geological exploration and can be much lower, up to units of gigawatts. In this case, the funds released go to the construction of alternative energy sources.
Energy-storage system
The storage system has three levels:
Primary level—long-duration storage at the terminals
- It is located on 40 terminals. It provides energy storage for one run (360 GWh] with a reserve.
| Storage type | Unit cost | Source |
|---|---|---|
| Gravity storage | $50–100/kWh | The Energy Vault practice: 25 The MW/100 The MWh $7.7 That's a million dollars.77/ kWh of CPD 75–85%, service life 30–40 years. |
| Pumped hydro / micro-hydro based on the HTMC | $80–150/kWh | Uses the natural elevation difference along the route. |
| BESS (lithium-ion) | $125/kWh (full setup) | According to Ember (2025): $75/kWh equipment from China + $50/kWh. installation. 215 GWh may decrease to $100- What? |
- The total capacity of the primary level: 360 GW·h (full cycle of displacement).70% of the gravity/GAS, 30% BESS) value:
| Component | Capacity | Unit cost | Cost |
|---|---|---|---|
| Gravity storage + pumped hydro | 250 GWh | $60/kWh | $15 billion |
| BESS | 110 GWh | $125/kWh | $13.75 billion |
| Total primary level | 360 GWh | $28.75 billion |
- The range of uncertainties: $22–35 billion.
Secondary level—buffer storage beside the tunnel windings
- Machines (inertia accumulators): are located directly by the wrappers and are used to smooth transition processes.0.5–1 For buffered cavities 1–5 GWh $0.5–5 billion .
Pulse level—microsecond stabilisation
- Ionistors (supercapacitors): Their function is to compensate for microsecond pulses and stabilize voltage when the load jumps sharply. 1% of the power output (1–3 (GW) With the relative value of the pulse systems $300–500/kWt·h $0.3–1.5 billion.
Total storage-system costs
| Level | Technology | Capacity | Cost (USD billions) |
|---|---|---|---|
| Primary | Gravity + pumped hydro + BESS | 360 GWh | $22–35 |
| Buffer | Flywheels | 1–5 GWh | $0.5–5 |
| Pulse | Ionistors | 1–3 GWh | $0.3–1.5 |
| Total storage | $22.8–41.5 |
Industrial centres and logistics
| Cost item | Cost (USD billions) | Basis |
|---|---|---|
| Industrial centre in Gabon—shuttle and launch-module production | $3–6 | Shipbuilding docks, factories and cranes |
| Industrial centre in the DR Congo—gateway and high-speed modules | $2–4 | Highland cluster and electrolysis system |
| Port development in Gabon and at Lake Tanganyika | $1–3 | Berths, cranes and warehouses |
| LEP and roads along the route (2050 km) | $4–8 | LEP 220 kV, highways, bridges |
| Hydro-Thermal Main Canal (HTMC) | $2–5 | Excavation, lining and locks |
| Total | $12–26 |
R&D and prototyping (Phase 0)
| Cost item | Range (USD billions) | Basis |
|---|---|---|
| Mathematical and CFD modelling | $0.01–0.03 | Analog: development of digital doubles for the hyperloop (CHF 4.5 million). |
| Geological survey of the route (2050 km) | $0.015–0.025 | $7,000–12,000/km for detailed reconnaissance in hard-to-reach areas. |
| Engineering and BIM documentation | $0.02–0.05 | Preparation of requirements, conceptual designs and detailed designs. |
| Test facility for the gateway and superconductors | $0.01–0.03 | A rig for the prototype gateway chamber and levitation modules. |
| Consortium formation and legal agreements | $0.005–0.015 | International negotiations, registration and insurance. |
| Total phase 0 | $0.06–0.15 |
- The $0.06–0.15 billion R&D budget is not fixed. If more deeply worked, a full-size prototype of the gateway was built, or large-scale testing on the stand could cost $0.5–3.0 billion. Therefore, the CAPEX table shows the range of $0.1–3 billion, and the median value is accepted for $1.5 billion.
Final consolidated project CAPEX
| Cost item | Range (USD billions) | Median (USD billions) | Share of CAPEX (%) |
|---|---|---|---|
| Tunnel excavation | $77.4–124.8 | $101.1 | 41% |
| TBM fleet and manufacturing | $2.64–4.84 | $3.74 | 1.5% |
| GATES (40 stations at 2.5 GWt) | $80–120 | $100 | 40% |
| Accumulation systems (3 level) | $22.8–41.5 | $32.2 | 13% |
| Industrial centres and logistics | $12–26 | $19 | 8% |
| R&D, licences and administration | $0,1–3 | $1.5 | 0.6% |
| Reserve for unforeseen (15%) | $31–49 | $40 | 16% |
| TOTAL CAPEX | $225–365 | $295 | 100% |
- Key conclusion: The median cost of the StarRoad project is about $300 billion.
Allocation by phase (USD billions)
| Cost item | Phase 0 | Phase 1 | Phase 2 | Phase 3 | Phase 4 | Phase 5 |
|---|---|---|---|---|---|---|
| Tunnel excavation | — | — | $5 | $20 | $70 | $6 |
| TBMs | — | $2 | $0.7 | $0.8 | $0.2 | $0.1 |
| GATES | — | $60 | $20 | $20 | — | — |
| Storage | — | $10 | $10 | $8 | $3 | $1 |
| Industrial centres + logistics | — | $5 | $3 | $3 | $5 | $3 |
| R&D and licences | $1.5 | $0.2 | $0.1 | $0.1 | $0.05 | $0.05 |
| Reserve (15%) | $0.23 | $11.6 | $5.8 | $7.8 | $11.7 | $1.5 |
| TOTAL by phase | $1.73 | $88.8 | $44.6 | $59.7 | $90 | $11.7 |
| Cumulative total | $1.73 | $90.5 | $135.1 | $194.8 | $284.8 | $296.5 |
Payback and the evolution of launch cost
- All data in this subsection are strictly theoretical.
Evolution of launch frequency and cost per kilogram
- StarRoad does not reach full capacity immediately. Launch frequency and payload-delivery cost evolve as additional lines enter service, the shuttle fleet expands and orbital infrastructure is deployed.
- Model of delivery-cost evolution in USD/kg to GEO and above:
| Period | Lines | Launches per year | Frequency | Delivery cost ($/kg) | Comment |
|---|---|---|---|---|---|
| Years 1–2 (pilot) | 1 | 12–24 | 1–2/month | $80–120 | First commercial launches. Operational development, high overheads and a small production series. |
| Years 3–5 | 1 | 50–100 | 1–2/no | $30–50 | The beginning of serial operation, the increase in the fleet to 3–5 vessels, the reduction in costs due to the scale effect. |
| Years 6–10 | 1 | 200–300 | ~1/day | $10–20 | The first line reaches design capacity. Maintenance is fully automated. |
| Years 11–15 | 2 | 500–700 | ~2/day | $3–8 | A second line enters service. Fixed costs are shared between two accelerators. |
| Years 16–25 | 3–4 | 1000+ | 3–5/day | $0.8–3 | Scalable to parallel lines 3–4. They have been developed with a capacity of >1 GW providing orbital energy for maneuvers and cargo processing. |
| Years of service 26+ | 5+ | 1500+ | 5–10/day | $0.3–1 | Mature infrastructure. Space power stations supply the accelerator and orbital factories. Energy becomes nearly free. |
Calculation of launch cost per kilogram
- Formula for each period: Ckg = (Cenergy + Cmaintenance + Cdepreciation + Coperations) / Mpayload, where:
- Cenergy is the cost of electricity, including cooling and auxiliary systems.
- Cmaintenance is maintenance of shuttles and infrastructure.
- Camort depreciation of capital costs (CAPEX, $300 billion, depreciation period 50 years).
- Coperations is other operating expenditure, including staff, logistics and insurance.
- Mpn mass of useful load per single launch (10 000 t).
- Resulting parameters by period:
| Period | Launches/year | Energy ($/kg) | Maintenance ($/kg) | Depreciation ($/kg) | Operations ($/kg) | Total cost ($/kg) |
|---|---|---|---|---|---|---|
| 1–2 year | 12 | 1.8 | 6.63 | 50 | 3.57 | 62 |
| 3–5 year | 50 | 1 | 1.25 | 12 | 0.67 | 14.92 |
| 6–10 year | 250 | 0.36 | 0.23 | 2.4 | 0.13 | 3.12 |
| 11–15 g (2 line) | 600 | 0.12 | 0.113 | 1 | 0.061 | 1.29 |
| 16–25 g (3–4 line) | 1200 | 0.045 | 0.049 | 0.5 | 0.026 | 0.62 |
| 26+ years (5+ lines + CSE) | 2000 | 0.015 | 0.015 | 0.3 | 0.008 | 0.34 |
Launch-cost structure in absolute figures
- For the average year in each period (for example 10 000 t of useful load):
| Period | Number of launches | Energy per launch (USD millions) | Maintenance (USD millions) | Depreciation (USD millions) | Operating expenditure (USD millions) | Total per launch (USD millions) |
|---|---|---|---|---|---|---|
| 1–2 year | 12 | 18 | 66.3 | 500 | 35.7 | 620 |
| 3–5 year | 50 | 10 | 12.5 | 120 | 6.7 | 149.2 |
| 6–10 year | 250 | 3.6 | 2.34 | 24 | 1.26 | 31.2 |
| 11–15 year | 600 | 1.2 | 1.13 | 10 | 0.61 | 12.93 |
| 16–25 year | 1200 | 0.45 | 0.49 | 5 | 0.26 | 6.2 |
| 26+ g | >2000 | 0.15 | 0.146 | 3 | 0.079 | 3.38 |
Key calculation assumptions
- Energy: the base price $0.05/kWh for the first years; by 26+ year it drops to $0.005/kWh thanks to the CSE and its own geothermal power.
- Tech-service (TO): in the pilot period high (repair, repair, overcrowding); by the 10 year automated conveyor TO.
- Amortization: CAPEX $300 billion is distributed over 50 years → $6 billion/year. At 250 launches/year it is $24 million/launch. Either the same annually compensated CAPEX ($6 billion/year) is counted as a constantly growing investment stream directed at building new StarRoad branches.
- CSES (Space Solar Power Plants): starting in 16 year, provide energy to orbital plants and partially to the accelerator, reducing energy costs and increasing sales revenue by orders of magnitude.
Integrated dynamics: revenue versus cost
| Period | Launches/year | Average market price ($/kg) | Launch revenue (USD billions/year) | Cost (USD billions/year) | Gross profit (USD billions/year) |
|---|---|---|---|---|---|
| 1–2 year | 12 | $100 | 12 | 7.44 | 4.56 |
| 3–5 year | 50 | $39 | 19.5 | 7.45 | 12.04 |
| 6–10 year | 250 | $9.6 | 24 | 7.8 | 16.2 |
| 11–15 year | 600 | $3.9 | 23.4 | 7.76 | 15.64 |
| 16–25 year | 1200 | $1.6 | 19.2 | 7.44 | 11.76 |
| 26+ g | 2000 | $0.5 | 10 | 6.75 | 3.25 |
- Note: GATES's energy sales revenue ($35–44 billion/year) is not included in this table it goes in a separate stream, covering depreciation and operating costs of infrastructure.
Conclusion on cost dynamics
- StarRoad starts with a $80–120/kg (GSO and above) withdrawal price which is already 10–15 times cheaper than Falcon Heavy (NOO $1,400/kg) and comparable to the Starship's target price (NOO $200/kg). By the year 10, the price drops to $10/kg, and by the year 25 it drops to $1/kg. By the 30 year, with 5+ lines and support for the CCS, the price reaches less than $0.5/kg, making space resources (solar energy, asteroid metals) economically available to earth industry.
- The key conclusion: even in the pilot period StarRoad is competitive. 30 years.
Comparison with alternatives
| Project | Type | Investment (CAPEX / R&D) | Payback | Cost / LCOE | Note |
|---|---|---|---|---|---|
| StarRoad energy component: GATES + storage | Energy | $100–150 billion | 5–7 years (from energy sales) | $0.05/kWh | Geothermal generation and storage only. Can pay back as an independent power plant. |
| StarRoad transport component: tunnel, gateway and shuttles | Transport | $150–200 billion | 8–12 years (including cargo) | $1–10/kg | Accelerator, gateway and shuttles. Pays back through cargo delivery while using energy from the first component. |
| StarRoad complete system | Energy + transport | ~$300 billion | 8–12 years (total income) | $0.05/kWh and $1–10/kg | Integrated project. Revenue from energy and cargo. |
| Falcon Heavy development | Transport | ~$5 billion (R&D) | ~10–15 years (at commercial frequency) | ~$1,400/kg | Existing rocket. CAPEX here means development cost, not permanent infrastructure. |
| Starship development | Transport | ~$10 billion (R&D) | ~10–15 years (at the target market) | The goal is $200/kg, prospectively $50–100/kg | Under development. Investment is in R&D, not permanent infrastructure. |
| Grand Inga hydroelectric project, DR Congo | Energy | $80–100 billion | 15–25 years | $0.03–0.05/kWh | Large hydroelectric project. Energy only. |
| Large nuclear power plant (2 block, ~2.4 GW) | Energy | $15–20 billion | 20–30 years | $0.05–0.08/kWh | Typical nuclear power plant. Energy only. |
Economic conclusion
- The economic model shows that StarRoad is a CAPEX project with a median of about $300 billion.
- The GATES ($80–120 billion) is the most expensive component, but pays off as an independent energy project for 5–7 years.
- Tunneling ($77–125 billion) is a technologically viable task using serial TPCs and own production.
- The accumulators ($23–42 billion) are based on falling BESS prices ($125/kW·h) and gravitational systems with the best world practices in mind.
- The R&D ($0,1–3 billion) corresponds to real prototyping costs, not full-scale construction.
- Economic attractiveness: StarRoad generates $35–44 billion/year from energy sales alone at the base price of $0.05/kWh, By covering operational costs and ensuring a return on investment from energy exports before full space launches begin.