Habitat pressure shell: what breathable air does to the structure
Study 004 · Sketch · Concept study, not a built system.
Study 004 · Sketch · First published 2026-10-13 · Revised 2026-10-13
Question
What load does breathable air put on a Mars habitat?
Assumptions
- Cabin pressure101, 70.3 or 56.5 kPa (BVAD Rev 2, Table 4-1)
- OutsideMars mean surface pressure 0.636 kPa, so Δp ≈ cabin pressure; g = 3.71 m/s²
- Shapecylinder, radius 3 m (our assumption)
- Coverfrom Study 003
- Materialallowable stress and safety factor left as variables; no alloy strength is quoted
The numbers
Hoop stress σ_h = p r / t → wall t = p r / σ_allow Longitudinal stress σ_l = p r / (2t) Line load p r: 101,325 Pa × 3 m ≈ 0.30 MN/m (70.3 kPa → 0.21; 56.5 kPa → 0.17 MN/m) Illustrative wall, p = 101.3 kPa, r = 3 m (σ_allow values are placeholders, not material data): 50 MPa → 6.1 mm 100 MPa → 3.0 mm 200 MPa → 1.5 mm (before safety factor) End-cap force: 101,325 × π × 3² ≈ 2.9 MN Can soil hold the air in? overburden = ρ g h 2 m loose soil 1,500 × 3.71 × 2 ≈ 11 kPa 575 g/cm² cover 5,740 kg/m² × 3.71 ≈ 21 kPa soil depth to balance 101.3 kPa ≈ 18 m (56.5 kPa → 10 m) Net uplift, 160 m² habitat at 101.3 kPa under 575 g/cm²: (101.3 − 21.3) kPa × 160 m² ≈ 12.8 MN
Result
Modeled: the shell is a pressure vessel in tension, carrying about 0.30 MN per metre of wall at 101 kPa. Regolith is radiation shielding, not structure: a buried habitat at sea-level pressure pushes up about 13 MN through its anchors or floor.
Trade-offs
| Cabin atmosphere | Line load (r = 3 m) | Effect |
|---|---|---|
| 101 kPa, 21% O₂ | 0.30 MN/m | no pre-breathe for EVA; highest structural load |
| 70.3 kPa (10.2 psia), 26.5% O₂ | 0.21 MN/m (−31%) | for vehicles with contingency EVA |
| 57 kPa (8.2 psia), 34% O₂ | 0.17 MN/m (−44%) | NASA-recommended for frequent EVA. The higher oxygen fraction raises fire risk and limits which cabin materials can be used |
Atmosphere pairs from BVAD Rev 2 §4.1, citing Norcross et al. 2013.
Open problems
- Material choice and fatigue over thousands of pressure cycles (airlocks).
- Leak rate (BVAD nominal 0.02 kg/day per module).
- Thermal cycling around a −60 °C mean outside.
- Anchoring for about 13 MN of uplift.
What would change the answer
- Lower cabin pressure cuts structural load almost in proportion, at the cost of fire risk from the richer oxygen mix.
Sources
Status: Sketch is first-order arithmetic that may move by ±50%; Draft has full structure but uses an approximation we name; Study has every input sourced. Figures are rounded. Where a value is our assumption, the table says so. Errors are logged on Corrections; report one on Discord.