Figure 1

Figure 2

Supplementary data 1:

Figure 3

Figure 4

Supplementary data 2

“Best and worst case scenario” incorporating potential launch, transit and habitation strategies_
| Best Case Scenario | Worst Case Scenario | |
|---|---|---|
| Crew Selection | No radiosensitive genes Resistant to sleep deprivation and psychological stress | General crew selection |
| Solar Cycle Launch Time | Solar maximum | Solar minimum |
| Propulsion System | Chemical, nuclear and electrical | Chemical |
| Intravehicular Suit | Graphene suit ∼ 162mSv | No additional shielding ∼ 213.3mSv |
| SPE Warning System | Solar flare telescope | No solar flare telescope |
| On-Board Storm Shelter During A SPE | Fuel tank barrier ∼ 44mSV | No barrier ∼ 3614mSv |
| Location On Mars For Habitation | Hella Planitia | Olympus Mons |
| Depth Below Surface For Habitation | 3m below surface ∼3mSv/yr | Surface ∼300mSv/yr |
| Total Radiation Dose | ∼209mSv/yr | ∼4127.3mSv/yr |
Comparison of dose received behind liquid fuel tank and unshielded dose along with potential clinical effects experienced by astronauts from an unshielded exposure from an SPE_
| Organ | Dose Behind Liquid Barrier | Unshielde d Dose | Clinical Effect |
|---|---|---|---|
| Skin | 0.013Gy | 14.5Gy | Pain |
| Testes | 0.012Gy | 3Gy | Azoospermia |
| Heart | 0.012Gy | 8Gy | Coronary |
| Brain | 0.013Gy | 1.6Gy | Nausea/Vomiting |
| Lens | 0.013Gy | 7.5Gy | Cataract |