Chapter 3
📍 Lunar Base Site Selection
Chapter Overview: Choosing the location of a lunar base is central to its success. This chapter evaluates candidate locations such as the polar regions, lava tubes, and crater rims, and compares the advantages and disadvantages of each.
Site Selection Criteria
Key factors to consider when choosing a lunar base location. The priorities for water, sunlight, temperature, Earth communication, and landing zone follow WIA-SPACE-011 §4.1; the remaining rows are supplementary criteria used in this book:
| Criterion |
Importance |
Description |
| Water access |
Top priority |
Within 10 km of confirmed PSR water ice deposits (§4.1.1) |
| Sunlight |
Very high |
At least 70% annual sunlight, target 80-90%; below 70%, nuclear power is required (§4.1.2) |
| Temperature stability |
High |
Daily temperature variation below 150°C (§4.1.3) |
| Radiation shielding |
High |
Protection from natural terrain |
| Earth communication |
Medium |
Direct line of sight to Earth more than 50% of the time (§4.1.4) |
| Landing zone |
High |
Slope below 15° within 5 km, boulder coverage below 5%, clear approach corridor (§4.1.5) |
| Scientific value |
Medium |
Diversity of research targets |
1. South Pole: Shackleton Crater
Location and Characteristics
89.9°S
Latitude (nearly at the pole)
80-90%
Solar availability
Advantages
- Permanently shadowed region (PSR): Water ice is expected in the crater's permanently shadowed interior; the standard rates the water resource as excellent (§4.2), although the actual quantity has not been measured
- Peaks of eternal light: The crater rim receives sunlight almost constantly (80-90% of the year)
- Temperature stability: Relatively stable; the standard gives -50°C to -30°C for polar regions (§4.1.3) and -40°C to -20°C for the Shackleton rim (§4.2)
- Earth visibility: From elevated rim sites, Earth is above the horizon for part of each month, allowing direct communication for part of the time
- Scientific value: Enables study of water ice preserved for billions of years
Disadvantages
- Extreme terrain: The crater walls are steep and rugged
- Permanent darkness: The crater interior is always dark, making work difficult
- Low temperatures: The interior of the PSR is extremely cold, below -200°C
- Limited communication: No direct communication from inside the crater; a relay is required
Artemis III Landing Candidate
NASA's candidate landing regions for Artemis III, announced in 2022 and later refined, all lie within a few degrees of the south pole, and several are near Shackleton Crater. The concept assumed in this standard is to build a base on the crater rim and use robots to mine the water ice inside the crater.
2. North Pole: Peary Crater
Location and Characteristics
Excellent
Water rating (§4.2)
Advantages
- Water ice: Radar and neutron data indicate ice in north polar shadowed craters; the standard rates Peary's water resource as excellent
- Continuous sunlight: Surrounding peaks receive sunlight more than 85% of the year
- Large crater: Much wider than Shackleton, offering more area to prospect
- Flat areas: Some areas are favorable for landing and construction
Disadvantages
- Low priority: The south pole is the main target of the Artemis program
- Earth communication: As at the south pole, Earth sits low on the horizon
- Insufficient exploration: Less studied than Shackleton
3. Lava Tubes
Locations and Discovery
Beneath the lunar surface lie enormous lava tubes formed by ancient volcanic activity. Major locations:
- Marius Hills: A skylight (pit) discovered by Japan's Kaguya in 2009; the standard's preferred future site (§4.2)
- Near Philolaus Crater: Candidate lava channels identified from orbital imagery
- Mare Tranquillitatis pit: Radar analysis published in 2024 indicated an accessible cave conduit beneath this pit, in the same mare as the Apollo 11 landing site
Hundreds of m
Ceiling thickness
-20°C
Stable temperature (§4.2)
Advantages
- Radiation shielding: A thick rock ceiling provides near-complete shielding; the standard treats it as 100% GCR shielding (§5.2)
- Micrometeoroid protection: The ceiling protects against impacts
- Temperature stability: Nearly constant year-round (the standard assumes about -20°C)
- Spacious interior: Provides enormous natural living space
- Possible pressurized volume: Sealing sections of a tube to hold pressure has been proposed, but it is unproven; the pressure-vessel requirements of §5.1.1 still apply
- Expandable: The natural volume allows expansion with less structural construction
Disadvantages
- Difficult access: Transporting equipment and materials to the cave entrance is complex
- No solar power: Sunlight does not reach inside, so nuclear power is essential
- Communication blockage: No direct communication with Earth from inside the cave
- Exploration required: The internal structure and stability must be verified in advance
- Structural risk: The possibility of ceiling collapse must be assessed
Future Outlook: In the long term, lava tubes are among the most promising lunar habitats. A realistic approach is to build an initial surface base first and then develop a lava tube base as a second phase.
4. Equatorial Region
Representative Location: Tranquility Base (Apollo 11 Landing Site)
-173 to +127°C
Temperature range (§4.1.3)
Excellent
Earth communication
Advantages
- Earth communication: On the near side, Earth is always above the horizon, making communication easy
- Flat terrain: The mare (sea) regions are very flat
- Historical value: The area near the Apollo landing sites is a tourist attraction
- Easy access: Low-latitude sites are easier to reach from equatorial orbits
Disadvantages
- Lack of water: Unlike the polar regions, there is almost no water ice
- 14-day night: No solar power generation during the long night
- Extreme temperatures: +127°C by day, -173°C at night
- Energy problem: Batteries or nuclear power are essential during the night
The equatorial region is suitable for early short-duration visits, but it is inferior to the polar regions as a site for a permanent base.
5. Crater Rim
Concept
The edge (rim) of a deep crater offers unique advantages:
Advantages
- High elevation: Higher than the surroundings, increasing hours of sunlight
- Water access: Access to the ice inside the crater
- Vantage point: A wide field of view benefits exploration and communication
- Natural shielding: Terrain on one side partially blocks radiation
Disadvantages
- Sloping terrain: Construction and movement are difficult
- Stability: Risk of crater wall collapse
- Confined space: Limited room for expansion
Site Comparison and Recommendations
The scores for Shackleton, Peary, and lava tubes are those given in WIA-SPACE-011 §4.2. The equatorial and crater-rim scores and all star ratings are this book's own illustrative assessment.
| Location |
Water |
Sunlight |
Temperature |
Radiation |
Overall score |
| South Pole: Shackleton |
⭐⭐⭐⭐⭐ |
⭐⭐⭐⭐ |
⭐⭐⭐⭐ |
⭐⭐⭐ |
9.5/10 |
| North Pole: Peary |
⭐⭐⭐⭐⭐ |
⭐⭐⭐⭐ |
⭐⭐⭐⭐ |
⭐⭐⭐ |
9.0/10 |
| Lava tubes |
⭐⭐ |
⭐ |
⭐⭐⭐⭐⭐ |
⭐⭐⭐⭐⭐ |
8.5/10 |
| Equatorial region |
⭐ |
⭐⭐ |
⭐⭐ |
⭐⭐ |
5.0/10 |
| Crater rim |
⭐⭐⭐⭐ |
⭐⭐⭐⭐ |
⭐⭐⭐ |
⭐⭐⭐ |
8.0/10 |
Phased Development Strategy
Phase 1: Polar Surface Base (2026-2030)
- Small outpost on the rim of Shackleton Crater
- 4-6 crew members, 1-2 month missions
- Water ice mining trials
Phase 2: Permanent Polar Base (2030-2040)
- 10-20 permanent residents
- Full-scale ISRU operations
- Hybrid solar + nuclear energy
Phase 3: Lava Tube Base (2040+)
- Underground city for long-term habitation
- Scale of 100 or more people (§15.1)
- Complete radiation shielding
Conclusion
The area around Shackleton Crater at the lunar south pole is currently the top candidate site, because it combines access to water, near-continuous sunlight, and relatively stable temperatures. In the long term, however, lava tubes may become the preferred habitat.
The next chapter examines the technologies and methods for actually building a lunar base at the chosen location.