Mars Terraforming
Calculations: Mars Terraforming
TL;DR
- Main problem: Mars lost its magnetic field 4 billion years ago -> atmosphere is stripped by solar wind
- Solution: Orbital ring of superconducting magnets (100-1000 satellites, ~1021-1022 A·m²)
- Shield power consumption: ~100 GW continuous (comparable to Dyson Swarm output)
- Sequence: magnetic shield -> heating -> greenhouse effect -> liquid water -> biosphere
- Conclusion: Mars terraforming is a separate megaproject after completing Helios
The Mars Problem
| Parameter | Mars | Earth |
|---|---|---|
| Magnetic field | None (lost 4 billion years ago) | 25-65 µT |
| Atmosphere | 0.6% of Earth’s | 100% |
| Temperature | -60°C average | +15°C |
| Water | Frozen | Liquid |
Without a magnetic field: - Solar wind strips atmosphere (~100 g/s) - Surface is irradiated - Any created atmosphere will escape
Why Heat the Planet?
Terraforming Logic
Step 1: Magnetic shield
↓
Atmosphere stops escaping
↓
Step 2: Heating with mirrors
↓
CO₂ in polar caps sublimates
↓
Step 3: Greenhouse effect
↓
Temperature rises -> more CO₂ sublimates
↓
Step 4: Ice melts
↓
Liquid water on surface
↓
Step 5: Biosphere
↓
Plants produce oxygen
What Mars Has
| Resource | Amount | Location |
|---|---|---|
| CO₂ (frozen) | ~4 trillion tons | Polar caps |
| Water ice | ~5 million km³ | Poles + subsurface |
| CO₂ (bound) | ~100 trillion tons | In rocks |
Problem: All of this is frozen at -60°C. Heating required.
Magnetic Shield: The Serious Option
Why Not a Dipole at L1
NASA concept (2017) - minimalist dipole at L1 point: - Power: ~150 MW - Problem: This is an “umbrella”, not a full magnetosphere - Does not protect from cosmic rays - Does not create radiation belts
Full Magnetosphere
Option: Orbital ring of superconducting magnets
| Parameter | Value |
|---|---|
| Orbit | Equatorial, 400-1000 km |
| Number of satellites | 100-1000 |
| Magnetic moment (total) | ~1021-1022 A·m² |
| Surface field | ~10-50 µT |
Comparison:
Earth: 8 × 10²² A·m² (at core) -> 25-65 µT at surface
Our shield: orbital ring closer to surface
Refined calculation:
For 10 µT field at surface from 500 km orbit:
m ≈ 3×10²¹ A·m² (30× higher than initial estimate)
Note: Calculation requires refinement - geometry differs from point dipole for orbital ring. Order of magnitude: 1021-1022 A·m².
Shield Power Consumption
Each satellite:
- Superconducting coil: current ~10⁶ A
- Cryogenic cooling: ~10-100 MW
- Mass: ~50-100 tons
1000 satellites:
- Total cooling power: 10-100 GW
- Total mass: 50,000 - 100,000 tons
Shield energy: ~100 GW (continuous)
Heating the Planet
Goal: Sublimate Polar Caps
CO₂ mass in caps: 4 × 10¹⁵ kg
Heat of sublimation CO₂: 571 kJ/kg
Energy for sublimation: 4 × 10¹⁵ × 571 × 10³ = 2.3 × 10²¹ J
At 500 TW power:
Time = 2.3 × 10²¹ / 5 × 10¹⁴ = 4.6 × 10⁶ seconds ≈ 53 days
BUT: also need to heat ice from -120°C to -78°C (sublimation point)
Add ~30% -> ~70 days
Conclusion: At 500 TW of directed heat - polar caps sublimate in ~2-3 months.
How to Direct Heat
Dyson Swarm mirrors redirect sunlight to Mars poles:
- 500 TW = ~6 million mirrors (100×100 m each)
- This is ~2.5% of the Swarm by year 3
Greenhouse Effect
After CO₂ Sublimation
Current Mars pressure: 0.6 kPa (0.6% of Earth's)
+ 4 trillion tons CO₂: +10-20 kPa
New pressure: ~10-20 kPa (10-20% of Earth's)
CO₂ greenhouse effect:
Δt ≈ 5-10°C per doubling of concentration
At 10-20 kPa CO₂: +30-50°C
New average temperature: -60 + 40 = -20°C
Still cold, but ice at equator will start melting in summer.
Enhancing Greenhouse Effect
For further heating: 1. Continue heating with mirrors (+10°C) 2. Add other greenhouse gases (SF₆, CF₄) 3. Release bound CO₂ from rocks (heating)
Terraforming Timeline
Aligned with prologue events (2075).
| Project Year | Calendar | Event | Result |
|---|---|---|---|
| 0 | ~2030 | Landing on Mercury | - |
| 3 | ~2033 | Swarm operational (9,500 TW) | Energy available |
| 3-25 | 2033-2055 | Priority: Earth | Energy bridge, infrastructure |
| 25-30 | ~2055-2060 | Shield construction | 100,000 t delivered |
| 30 | ~2060 | Shield activation | Atmosphere stops escaping |
| 30-35 | 2060-2065 | Polar heating | CO₂ sublimates |
| 35-40 | 2065-2070 | Greenhouse acceleration | Temperature rises |
| 40 | ~2070 | Mask instead of spacesuit | Pressure 10-15 kPa |
| 42 | 2072 | First lake | Liquid water! |
| 45 | 2075 | 200,000 colonists | Domed cities |
| 70-100 | 2100-2130 | Comfortable climate | 0°C average |
| 150-300 | 2180-2330 | Breathable atmosphere | 21% O₂ |
Terraforming Energy Budget
| Task | Power | % of Swarm | Duration |
|---|---|---|---|
| Magnetic shield | 100 GW | 0.001% | Continuous |
| Cap sublimation | 500 TW | 5% | 2-3 months |
| Heat maintenance | 500-1000 TW | 5-10% | 100+ years |
| Water electrolysis (O₂) | 100 TW | 1% | Continuous |
| Industry | 50 TW | 0.5% | Continuous |
Total for Mars: ~15-17% of Swarm power
Comparison with Swarm
| Parameter | Value |
|---|---|
| Swarm power (year 3) | 9,500 TW |
| Mars consumption | ~1,500 TW |
| Remainder for other projects | ~8,000 TW |
Mars consumes 15% of the Swarm.
The remaining 85% available for:
- Earth energy supply
- Other planets (Venus, moons)
- Interplanetary logistics
- Space industry
Realistic Expectations
What’s Possible in 100 Years
| Parameter | Now | In 100 years |
|---|---|---|
| Pressure | 0.6 kPa | 30-50 kPa |
| Temperature | -60°C | 0 - +10°C |
| Water | Ice | Lakes, rivers |
| Atmosphere | 95% CO₂ | 95% CO₂, trace O₂ |
| Life | None | Plants under domes |
What’s Needed for “Breathable” Atmosphere
Needed: 21% O₂ at 100 kPa = 21 kPa oxygen
Mass: ~5 × 10¹⁶ kg O₂
Source: Water electrolysis
2H₂O -> 2H₂ + O₂
Energy: 286 kJ/mol O₂ = 9 MJ/kg O₂
For 5 × 10¹⁶ kg:
E = 5 × 10¹⁶ × 9 × 10⁶ = 4.5 × 10²³ J
At 100 TW: time = 4.5 × 10²³ / 10¹⁴ = 4.5 × 10⁹ s ≈ 140 years
Conclusion: Even with a Dyson Swarm, creating a breathable atmosphere takes ~150-500 years.
Summary
| Stage | Project Year | Calendar | Requirements |
|---|---|---|---|
| Magnetic shield | 25-30 | 2055-2060 | 100 GW + 100,000 t |
| CO₂ sublimation | 30-35 | 2060-2065 | 500 TW × years |
| First lake | 42 | 2072 | Greenhouse effect |
| Comfortable climate | 70-100 | 2100-2130 | 1000 TW continuous |
| Breathable atmosphere | 150-300 | 2180-2330 | 100 TW for electrolysis |
Why Not Sooner?
First 25 years (2033-2055) priority is Earth: - Building photoreceiver stations - Deploying Energy Bridge - Solving Earth’s problems (hunger, energy, ecology)
Mars is the second priority. Only after Earth stabilization does large-scale terraforming begin.
Key conclusion: Mars terraforming is a centuries-long project, but the Dyson Swarm makes it possible. First lake in 2072 - 42 years after project start.
See Also
- Technologies and Sources - TRL of technologies, including magnetic shield references
- Why Mercury? - location comparison
- Project in 5 Minutes - Swarm technologies
- Swarm Mirrors - energetics and efficiency
- Roadmap - project timeline