Radiation shielding

Water-shield Greenhouse Concept

Early explorers will simply accept the radiation dose for the 2.5 year round trip (which should give approximately a 1% lifetime increase of a fatal cancer). See "The Case for Mars, chapter 5. However, radiation protection becomes much more of a concern for long durations habitats where people will live on Mars for years or decades. In such cases, thick shielding (of soil or ice), exotic modern materials, or electro-static or magnetic shields become more sensible. Radiation from the natural radioactive elements in the soil should be approximately equal to Earth doses. Radiation from Solar and Cosmic rays will be stronger, with the latter being much more difficult to shield against. See Cosmic Radiation.

General

The average radiation on Earth is very low at ~6.2 mSv / year. However, in some areas of the city Ramsar, Iran, the radiation level is 260 mSv / year, with no increase in health problems. Thus the radiation safety levels in many countries on Earth, are likely too conservative. This is good news for Mars colonists, our goal is not 6.2 mSv per year, but say 200 to 250 mSv / year. The discussion below assumes we are aiming for 6.2 mSv, but there shouldn't be a disaster if this is missed, even by a significant amount.

Also note that sudden radiation doses are much more dangerous than a small steady dose over a long period of time. A solar storm is FAR more dangerous than the slow and steady trickle of cosmic rays.

Long term settlers will need to shield against 3 types of radiation: Electromagnetic radiation, Solar Cosmic Rays, and more powerful Cosmic Rays. Of the last, Galactic Cosmic Rays are by far the most common fraction of these.

Electromagnetic Radiation

The EM spectrum consists of radio waves, microwaves, heat, visible light, ultraviolet light, x-rays, and gamma rays. The low energy end of this spectrum are waves that pass thru us and are harmless. As the frequency becomes shorter, the energy of each particle of light increases. The high energy EM waves act progressively more like particles and can damage tissue. UV light can give sun burn and damage surface tissue, and X-rays and gamma rays can do deep tissue damage.

EM waves are stopped by atoms with many electrons. Thus heavy metals strongly mitigate them. Air, dust, soil, and water all reduce their effect. The only common dangerous EM radiation on Mars is Ultraviolet (UV) light. On Earth, the stronger UV rays are stopped by our ozone layer, on Mars, 95% of the UV light reaches the ground, sterilizing the top layers of soil. (Also note that Mars gets about half the UV light that Earth does, because Mars is further from the sun.)

UV light can make plastics brittle, which may not be a concern for an 18 month stay, but it will be a problem for long term settlers. Metals and certain composites are resistant to UV light. The space suits and habitat materials will be designed to shield against UV rays.

X-rays and gamma rays are much more penetrating. For example, compressed Martian soil will halve the amount of gamma rays for each 9.1 cm of soil. Water halves the gamma ray flux for every 18 cm.

That said, the sun produces few x-rays and almost no gamma rays. A tiny amount come from space. The amount is low and can be basically ignored.

If a Mars base has a local source of gamma rays, say a nuclear reactor, it must be properly shielded, far away, or both.

Solar Cosmic Rays

These are not the solar wind, but rather high energy particles (mostly protons) which are produced in Coronal Mass Ejections. Most are low energy, 50 kilo-electron volts (eV) or less. These are easy to shield against. However, fairly rarely, powerful CME release particles in the 200 mega-electron volt range are produced. Maybe once or twice a decade, particles reach the giga-electron volt ranges are reached. These very rare, super explosions will be discussed below.

Small CME happen all the time, about once a week at solar minimum. Not all of these burst of particles hit Mars, the vast majority will shoot off in some other direction. These small bursts are fairly easy to shield against, the Martian atmosphere giving significant protection, space suits a little protection, and the habitat (with thick shielding for Galactic Cosmic rays giving) excellent protection. Martian colonists will likely ignore these.

The more powerful CME (say from 10 to 200 m-eV) are the 'solar storms' which occasionally feature on the news. A big one happens a few times a year at Solar maximum. These are very dangerous on Mars. Lacking a magnetic field, the high energy protons can reach the surface, only slightly attenuated by the thin atmosphere. The fairly thick radiation protection on bases will not be enough. It will be deadly dangerous to be caught on the surface during a big solar storm.

With a few hours warning, Martians will go deep in the base, likely several meters underground (or under a few meters of water) to a Storm Shelter to hide for 2 to 4 hours that the solar storm is active. Since most Coronal Mass Ejections miss Mars (and if they happen at night time they are harmless) this would happen maybe 10 to 30 times in a human lifetime.

A super-CME in the giga-electron Volt range is like the above only worse. You are still safe at night. But if it happened during Martian day, people would go into the shelter and still take a significant dose of radiation. This might happen once in a lifetime, and the storm shelters should be designed to prevent lethal doses of radiation from reaching the people inside.

These only will give an hour or two warning, so people won't have a lot of time to beef up defences. The storm shelter you have is the one you get, so don't skimp in your preparations.

Note that if you are living in a habitat in a lava tube (likely dozens or scores of meters underground) you are completely safe.

Galactic Cosmic Rays

More powerful Cosmic rays come in 3 types: Galactic Cosmic Rays, Extra Galactic Cosmic Rays, and Extreme Energy Cosmic Rays. The latter two are so powerful that no amount of shielding will protect against them, we will accept the dose from these, just as we do on Earth. Fortunately they are so rare, that they don't add that much radiation in a lifetime.

But shielding against Galactic Cosmic Rays is a very difficult task. These range from millions to billions of electron volts, and come from every area of the sky, in a steady trickle all times. They are common enough to add significantly to a Martian's lifetime radiation exposure. Realistically, Martians will have to accept a higher radiation dose than on Earth, they are just too hard to shield against.

A proton or alpha particle cosmic ray of in the upper end of this energy range can pass through more than a meter of aluminium, not counting the effects of secondary radiation.

However, living on a planet halves the radiation dose compared to someone in space or in a space station. (The ground blocks half of the celestial sphere, providing thousands of km of shielding.) Living in a deep valley or near the bottom of a cliff, will also reduce this radiation load.

These particles are very hard to shield against. They are not deflected (enough) by magnetic fields; they punch right thru the Sun's and Earth's magnetic field and hit every part of Earth. A few cm of soil which reduces a gamma ray dose by 8 fold, would actually increase the damage from these particles since the impact will produce Secondary radiation. They can produce free neutrons (albedo neutrons) which are not directly dangerous, but will cause beta decays which are.

What you really want is thick masses of small atoms (such as hydrogen, helium, lithium, etc.) Water with 2 hydrogens is good. Plastics (with hydrogens clustered around carbon chains) are good. Lithium hydroxide (with both lithium and hydrogen) is good. As a bonus, these sorts of materials are very good at stopping albedo neutrons as well.

With this in mind, it is clear that any Martian colonists would have to take a holistic approach, reducing their radiation exposure at every possible opportunity through shielding and risk-mitigating behaviour.

Passive shielding

The Mars Foundation concept for a side-lit greenhouse.

Any matter placed between a person (or radiation-sensitive equipment) and a radiation source reduces the amount of radiation they absorb.

Mars One's solution is a thick layer of regolith on top of the settlement modules. An effective shield will require at least several hundred grams of regolith per square centimeter, according to one study. Using a regolith density estimate of 1.4 g/cm³, this means the regolith layer would need to be over 2 meters deep. For concrete with an average density of 2.4 g/cm3 the required thickness should be about 40% less.

Protection from Electromagnetic Radiation

The attenuation of radiation follows the Beer Lamberth law.

I_x=I_o*e^-ux

Where:	Ix	=	the intensity of photons transmitted across some distance x
	I0	=	the initial intensity of photons (or radiation in general)
	s	=	a proportionality constant that reflects the total probability of a photon being scattered or absorbed (TBC)
	µ	=	the linear attenuation coefficient
	x	=	distance traveled (thickness of material)

Linear Attenuation Coefficients (in cm^-1) for a range of materials at gamma-ray energies of 100, 200 and 500 keV.

Absorber	100 keV	200 keV	500 keV
Air	0.000195	0.000159	0.000112
Water	0.167	0.136	0.097
Carbon	0.335	0.274	0.196
Aluminium	0.435	0.324	0.227
Iron	2.72	1.09	0.655
Copper	3.8	1.309	0.73
Lead	59.7	10.15	1.64

the linear attenuation coefficient µ is not commonly found in the literature, the mass attenuation coefficient µ_m is usually used instead. The coefficient is also dependent on the type of radiation, so a complete solution for radiation protection requires multiple analysis of the type of radiation to be protected against.

Conversion is quite simple as:

µ=µ_m*density of the material

List of mass attenuation coefficients can be found at the NIST website. https://physics.nist.gov/PhysRefData/XrayMassCoef/tab3.html

Another common way of evaluating radiation shielding is to use the half value, that expresses the thickness of absorbing material which is needed to reduce the incident radiation intensity by a factor of two, or I_x=I_o / 2.

The Half Value Layer for a range of absorbers is listed in the following table for three gamma-ray energies:

Half Value Layers (in cm) for a range of materials at gamma-ray energies of 100, 200 and 500 keV.

Absorber	100 keV	200 keV	500 keV
Air	3555	4359	6189
Water	4.15	5.1	7.15
Carbon	2.07	2.53	3.54
Aluminium	1.59	2.14	3.05
Iron	0.26	0.64	1.06
Copper	0.18	0.53	0.95
Lead	0.012	0.068	0.42

The first point to note is that the Half Value Layer decreases as the atomic number increases. For example, the value for air at 100 keV is about 35 meters and it decreases to just 0.12 mm for lead at this energy. In other words 35 m of air is needed to reduce the intensity of a 100 keV gamma-ray beam by a factor of two whereas just 0.12 mm of lead can do the same thing. The Half Value Layer increases with increasing gamma-ray energy. For example, from 0.18 cm for copper at 100 keV to about 1 cm at 500 keV.

Also note that this table is for gamma rays. Gamma rays in the kilo-electron volt ranger are not the big problem. Giga-electron volt cosmic rays are.

Protection from Particulate Radiation

On Earth, particulate radiation is often easily addressed because the particles have low enough energies that they can be stopped by a thin shield. In space and on the surface of Mars, shielding needs to account for high-energy particles. When it comes to particulate radiation, the effectiveness of shielding increases with the mass of the shielding and decreases with the atomic mass of the elements used for the shielding. The reason that low-atomic-mass elements are advantageous is that they generate less secondary radiation when impacted by particles.

For example, 1kg of hydrogen offers more protection then 1kg of aluminium.

2kg of aluminium offers more protection than 1kg of aluminium.

Finally, 1kg of hydrogen offers more protection than 2kg of aluminium.

Also, particles interact with atomic nuclei, while electromagnetic radiation interacts with electrons. So while for electromagnetic radiations the effectiveness of shielding increases with the number of electrons, and therefore with heavier atoms that have more electrons, for particles the effectiveness of radiation protection increases with the number of nuclei per volume, and lighter materials such as hydrogen have more nuclei per volume.

This study looked at the cosmic ray protection of Martian regolith. It found that 1 meter of regolith would reduce cosmic radiation by 41%. So two meters would reduce the radiation load down to about 1/3.

Possible Shielding Materials

Comparison of Material Options

Material	Advantages	Disadvantages
Metal	Efficiency of using structural material for incidental shielding benefit; some metals block EM radiation very well	Secondary radiation
Plastic	High hydrogen content	Less structural utility than metal
Water	High hydrogen content	Liquid
Liquid hydrogen	Pure hydrogen	Cryogenic liquid
Lithium Hydroxide (LiOH)	Contains Li & H, both small molecules. Denser than water, best neutron absorber / kg.	Needs to be kept dry
Regolith	Obtainable through ISRU	Large thickness required for thorough shielding
Regolith plus epoxy	Mostly obtainable through ISRU; greater hydrogen content than regolith alone; more durable and easier to shape than regolith alone	More complex to implement than regolith alone
Boron nitride nanotubes	Low atomic numbers; boron absorbs secondary neutrons well compared to other elements; possible use as both shielding and structural material; hydrogen could be stored in or bonded to nanotubes to improve shielding	Difficult to manufacture

Active shielding

For a Martian stay of 18 months, elaborate precautions are not needed. If people are going to spend many years on Mars, active shielding becomes more important.

Active shielding against radiation involves a man-made electromagnetic field which deflects ionized particles in a similar manner to the Earth's magnetic field. Several different types of active shield have been proposed, including electric field, magnetic field, and plasma shield designs. Such fields might require infeasible amounts of energy to generate (a Mars temperature superconductor would be useful here). Such a magnetic shield could also pose a risk to anyone approaching the craft or base, as it would create bands of trapped particles similar to the Van Allen belts. However, the radiation exposure might be low, as traversing the magnetic shield should be a very brief event. (If these 'van Allen belts' cross into the ground, charged particles would be absorbed and the issue won't arise. For a fixed base, one pole could be in the air, and one underground.)

It might be possible to situate a base in such a location that one of the residual Martian magnetic fields offers a net benefit. Care should certainly be taken not to situate it where the fields concentrate radiation.

Also, it might be possible (assuming one could generate the required magnetic field in some way) to have the radiation belts of the habitat pass through some sort of physical barrier, which scrubs them of particles.

Note that magnetic shields are good against lower energy particles, they are of little help against high energy Cosmic Rays. However, every bit helps, so these ideas may help in a 'layered defence'.

Design concepts

Protection during transit to Mars

A straightforward approach to designing an active shield would be to surround the protected space with a spherical enclosure made of a conducting metal that is held at a positive electric charge.  Solar radiation both consist of positively charged particles, which would be repelled by the positively charged shield. Positively charged cosmic rays have too much energy to be deflected by such a shield. To protect science experiments from cosmic rays on Earth, scientists go deep underground. They do not make a small metal charged dome.

One drawback to this concept is that the shield would attract free electrons and accelerate them, creating secondary radiation when they impact the shield.  These electrons would also drain the shield's positive charge, increasing the power needed to maintain it.

This led to the idea of adding a negatively-charged outer shield to keep electrons away from the positively-charged inner shield.  However, this introduces its own problems:  the mass requirement increases substantially, and the two shields must be tightly fixed in precise concentric positions, because any asymmetry would result in a strong attractive force that would pull the two shields together.

More recent concepts have moved away from the idea of enclosing the protected space in a charged shell.  A 2006 paper described a design in which trusses extended out from a spacecraft in the x, y, and z directions.  The trusses are used to suspend individual sphere-shaped charge centers:  positive charges are held 50 m from the spacecraft, and negative charges are 160 m out.  These charges are meant to generate an electric field sufficient to deflect incoming ions approaching from any direction.  Despite the elimination of the enclosing shells, the authors concluded that the mass requirement was still too high for this design to be practical.

In 2011, a concept using toroidal (doughnut-shaped) rings as charge centers was studied.  Three conductive rings, each with a 45 m radius, are positioned with their axes of symmetry along the x, y, and z axes, and held at a positive voltage.  In addition, six negatively-charged spheres are suspended from trusses, 160 m out.  For comparison, the researchers ran simulations of this design and a similar design that used only spherical charge centers.  Both designs offered good protection from SPE.  The toroid design was more effective against GCR.  Ring thicknesses of 1, 5, and 10 m were simulated, showing effectiveness against GCR increasing as a function of thickness.  To minimize the mass of the shield, the use of an electrostatically inflated membrane structure was proposed for the charge centers: instead of using a rigid metal, the charge center surfaces would be made of a flexible membrane with a conductive coating.  Unlike a balloon that is inflated by filling it with a gas, this type of structure would inflate to its intended shape when electrically charged because of repulsion between like charges distributed across the membrane.

A 2012 paper by Westover et al. described a design that used a magnetic field.  The field could be generated by multiple layers of superconducting material wrapped around a cylindrical spacecraft in double-helix-shaped coils.  Their simulations of this design found that a large, weak field was easier to generate than a small, intense field of equivalent shielding effectiveness. They also examined another design, a cylindrical spaceship surrounded by six exterior solenoids, each centered on a separate central axis (unlike the double helix design, in which the magnetic coil and the spacecraft are co-axial).  To reduce the magnetic field inside the spacecraft, a compensation coil, with a current moving in the opposite direction, would surround it.  Overall this design was judged to be preferable to the double helix design. Shortcomings of the latter design include the fact that the multiple layers of coils make it difficult to design a shield that can be compacted for launch and later expanded in space.  In addition, it would be more difficult to block the magnetic field intruding into the spacecraft because the field strength varies more at different points within the spacecraft; problems might also arise from forces created by the magnetic field acting on the shield or spacecraft.

Minimagnetosphere

A minimagnetosphere may be a viable alternative to the strong local magnetic fields described above for spacecraft. Minimagnetospheres have been detected on the Moon, and indications show that they have modified the interactions of the solar wind with the surface. The concept uses an electric field rather than the magnetic field. An plasma cloud is created around the vehicle by injecting charged particles and kept in place using a small superconducting magnet at the vehicle. The electrical charge can deflect particles due to the large size on the minimagnetosphere, that can reach a number of km in diameter. This solution might be particularly applicable to a cycler type vehicle.

The mass required to generate such a mini-magnetosphere must be low, or people will do without and accept the modest radiation exposure for such a trip.

Risk-mitigating behaviour

The possible sources of radiation on Mars are man-made sources, (such as nuclear reactors or medical equipment), solar radiation, galactic cosmic radiation and naturally occurring radioactive elements on Mars.

Living in a deep lava tube takes care of the problem. However many sites on Mars do not have these. For those areas...

Possible behavioral choices which minimize the risk from these include:

• Avoiding daytime EVA during solar storms.
• Working preferentially close to natural or man-made objects, such as habitats, rovers or cliffs which provide additional (if not omni-directional) shielding. For example, if a habitat was at the base of a tall cliff, then half of the cosmic rays, and half the high energy solar radiation would be shielded from.
• Entering a storm shelter when there is a high-radiation risk from solar particle events.
• Placing blocks of ice around the outer walls of the base is an excellent radiation shield.
• Sandbags on the roof of the habitat provide excellent solar protection, and minor protection verses high energy cosmic rays.
• Sleeping in areas with higher radiation protection. e.g. under bladders at ceiling filled with local water.

Example of using shielding and behavior to reduce radiation dosage

We can combine passive shielding with risk mitigating behavior to achieve low radiation exposure but still allow for some views of the exterior through windows. For example:

• Martian background average radiation is 240-300 mSv per year.
• If you sleep in a radiation shielded space such as underground rooms with a compacted regolith cover several meters thick, 8/24 hours, then the dose would go down by 1/3, to 160-200 mSv per year.
• If you spend most of your living (work, study) time in a radiation shielded space, then your dose becomes another 1/3 less, or 80 to 100 mSv.
• With overhangs and a radiation proof roof, 70% of the incident radiation to a space close to windows can be stopped by geometries, then the dose is down to 20 to 25 mSv.  this is about the 20 mSv per year for a 5 year period that is recommended for radiation workers.
• Part of the surface dose on Mars is solar proton events (SPE).  These are predictable and detectable, and a large settlement will mostly be built of shielded areas.  So during Solar Proton Events you should stay away from the windows. This behavior might reduce the yearly radiation load another 25%, down to 15-18 mSv per year. (If people go into a storm shelter for the worst solar storms, the dose would be reduced further.)
• What is the portion of the dosage from SPE?  I have a weak reference that puts this at 30%.  If correct, then the radiation load from large windows under a radiation proof ceiling is acceptable.
• Mars should be low in radon because it seems to be low in Thorium and, by analogy, Uranium as well. However, the habitats are totally enclosed spaces and radon generated by radioactive decay of naturally occurring uranium in the soil might accumulate. As 1 to 3 mSv on Earth comes from atmospheric radon, this part of the yearly load might go away, just as it might need to be mitigated if radon accumulates in the enclosed habitats.
• Even just 1/2 to 1 inches of glass reduces radiation dosage significantly.

If the above is correct, then large windows are not really an issue.  Geodesic glass domes over public spaces might be a poor choice, unless there is an understanding that you don't spend more than 2 to 4 hours per day under them.

Bibliography

"The Case For Mars", by Robert Zubrin, Simon and Schuster, ISBN 978-1-4516-0811-3. Chapter 5 has a very nice breakdown of radiation exposure from Conjunction and Opposition class missions.