A close view of the station hull with shielding cassettes, repair seams, maintenance rails and a launch trench.

Radiation and debris

Space is full of fast particles and drifting rocks. Concordia answers with mass: a thick layered shell of regolith and water, shelters for solar storms, and a layered watch for anything big enough to matter.

What the tags mean

Two kinds of radiation

Space radiation comes in two kinds, and they need different answers.

galactic cosmic rays are a constant rain of fast protons and heavy atomic nuclei from outside the solar system. They arrive from every direction all the time. They are strongest when the Sun is quiet. Thin shielding does little against them, because a cosmic ray that hits a wall breaks into a shower of smaller particles. NASA puts the average cut from aluminium or polyethylene at about 7 percent. Established physics

A solar particle event is a storm. The Sun throws out a burst of protons that is lower in energy than a cosmic ray and easier to stop. Storms are infrequent and peak around solar maximum. The same NASA brief says 5 to 20 grams per square centimetre of aluminium or polyethylene works against them, and that warning plus a shelter is the main defence. Established physics

Mass is the shield

The best shield is a lot of stuff. Earth wears one: the air above your head is about 1,000 grams of material over every square centimetre. A spacecraft has a few grams. NASA recommends at least 20 g/cm² for missions longer than six months. Established physics

Concordia has the Moon. A layer of regolith one metre thick at 1.6 tonnes per cubic metre is 160 g/cm², eight times NASA's guideline for a long mission. Covering the 470 km² of the station's surface at that thickness takes about 750 million tonnes. Design value That is why the station was built factory-first: asteroid haulers brought the first metal, and lunar mining and a mass driver were running at scale ahead of the first rotor (see how Concordia was built). Story

The shield stack above a Concordia rotor Seven layers from outside to inside, not to scale. A thin sacrificial impact layer, a vacuum standoff, a thick layer of regolith and slag cassettes, the structural shell, a service vacuum, a hydrogen-rich water layer, and the rotating pressure vessel that holds the air. Debris and radiation arrive from the top. Debris, cosmic rays and solar protons arrive from space vacuum 1 m of regolith = 160 g/cm² 1.6 t per square metre vacuum Air at Earth sea-level pressure city, 1 g at the ground 1. Sacrificial impact layerBreaks up small debris first 2. Standoff vacuumLets fragments spread out 3. Regolith and slag cassettesBulk mass: stops debris, thins radiation 4. Structural shellCarries the load 5. Service vacuumRoom for robots and plumbing 6. Hydrogen-rich waterThickest over beds, clinics, shelters 7. Rotating pressure vesselHolds the air; hundreds of metres inward Not to scale. Thickness is set by particle-transport analysis; 1 m is the scale example.
Seven layers from space to the air: impact layer, vacuum, regolith cassettes, structural shell, service vacuum, water, pressure vessel.

The stack has seven layers. A sacrificial layer on the outside breaks up small debris. A vacuum gap lets the fragments spread. The thick regolith and slag cassettes stop what is left and thin the radiation. A structural shell carries the load. Behind it lies a service vacuum for robots and plumbing, then a layer of water and other hydrogen-rich material, which stops particles well. The rotating pressure vessel with the air is the last layer, hundreds of metres inward. Design value

The thickness is not one number. Particle-transport calculations set it, and the shield is thickest where people sleep or heal: over bedrooms, hospitals, command centres and shelters. The 1 m example gives the scale.

The shield has gaps by design. The open industrial bay and the shipyard cage are not shielded, because robots do most of the work there and people go in pressurised capsules. And there are no large windows to space anywhere in a rotor. A window is a hole in the shield. The sky overhead is a display. Design value

A close view of the station hull with shielding cassettes, repair seams, maintenance rails and a launch trench.
Up close the shield is a mosaic of regolith and slag cassettes, with repair seams and a rail for the crawlers that swap them. Open this view in the simulation
The hull up close with the shielding overlay naming regolith and slag cassettes, the standoff vacuum and the open industrial bay.
From 5 km with the shielding overlay: the same cassettes form the outer layer, with a standoff vacuum behind. The open industrial bay is one of the shield's two planned gaps. Open this view in the simulation

Open in the simulation: Exterior Hull: Close Inspection Open in the simulation: Shielding overlay

Storm shelters

A solar storm is stopped by shelter, not by thickness everywhere. People who are away from the thickest shielding go to a dedicated storm shelter when the alert sounds. Concordia has them in the terminal citadel and at the roots of the piers. Pressure refuges along the stationary spine cover a different emergency, a loss of air. Safety shows how the refuges, pressure districts and shield fit together. Design value

NASA's rule of thumb gives the scale. A vehicle with 20 g/cm² of aluminium keeps a once-in-a-decade storm under the limit. For a storm that comes once in a century, add a shelter with 10 cm of water or its equivalent. For one in a thousand years, add 20 cm. About 95 percent of storms never approach dose limits. Established physics

The numbers on the other side matter too. NASA limits an astronaut's whole career to 600 millisieverts and a single storm to 250. The 1975 NASA settlement study set a design target of 0.5 rem a year, 5 millisieverts, for the general population of a settlement. A city of children has a stricter standard than a mission. Design value

Pier 1 on the outer face of the end bulkhead with a freighter alongside and tugs working near the axial approach.
A freighter alongside a spaceport pier on the outer face of the end bulkhead. Storm shelters sit at the pier roots. Open this view in the simulation

Open in the simulation: Spaceport External Pier Open in the simulation: A pressure refuge in the spine

Debris

Small rocks are rarely a surprise. The engineering question is how big. Around Earth, radar tracks objects larger than about 10 cm. Between 1 and 10 cm, objects are numerous and not individually tracked. Below 1 cm, shielding handles them. The International Space Station withstands impacts up to about 1 cm on its critical parts. Established physics

The trick behind that shielding is the Whipple shield: a thin outer bumper spaced out from the wall. The bumper breaks a fast projectile into a cloud, and the cloud spreads its energy over a wide patch of the wall behind. Concordia's thick stack works this way. The 1 to 10 cm range, which a catalogue cannot see and a thin shield cannot stop, is covered by metres of sintered regolith with bumper layers in front.

Anything larger than 10 cm gets a watch. Four defence sites, two at each end of the station, carry radar fences, an 85 m tracking dish, survey telescopes and lidar masts. Launcher batteries behind them hold heavy interceptors, rapid interceptors, point-defence guns and net launchers. The logic is layered detection and intercept, not shooting every particle. Directed-energy weapons are left out on purpose. The cargo mass drivers stay separate from defence, and incoming shipments from the Moon and asteroids are caught tens to hundreds of kilometres away, never aimed at the habitat. Engineering challenge

The forward defence battery on the hull: an armoured housing, reload magazine and interceptor cells under a black sky.
The forward defence battery: armoured housing, reload magazine and interceptor cells on the hull. Open this view in the simulation

Open in the simulation: Forward Defence Battery Open in the simulation: Defence overlay

What it feels like

Nothing. That is the point. The sky is a display, the shell is opaque and the air feels like air. You meet the shield in small ways: a shelter hatch in a terminal, a serial number stencilled on a cassette on a hull tour. A resident thinks about radiation about as often as anyone on Earth thinks about cosmic rays. Story

Go deeper: Shielding arithmetic Established physics

Shielding is measured in areal density, mass per unit area: ρ × t.

Regolith: 1,600 kg/m³ × 1 m = 1,600 kg/m² = 160 g/cm²
Station surface: A ≈ 470 km² = 4.7 × 10⁸ m²
Mass: 1,600 × 4.7 × 10⁸ = 7.5 × 10¹¹ kg = 750 million tonnes

For scale, a column of sea-level air is P / g:

101,325 Pa / 9.81 m/s² = 10,330 kg/m² = 1,033 g/cm²
Aluminium for 20 g/cm²: 20 / 2.7 g/cm³ = 7.4 cm
Water for 10 g/cm²: 10 cm
Reference Areal density
NASA guideline for storms, long missions 20 g/cm²
Storm shelter, extra for a 1-in-100-year storm 10 g/cm² (10 cm water)
One metre of regolith 160 g/cm²
Earth's atmosphere about 1,000 g/cm²
Go deeper: Worked example: what a small rock carries Established physics

A 1 cm aluminium sphere has a mass of ρ × 4/3 × π × r³ = 2,700 × 4.19 × (0.005)³ = 1.4 g. At an illustrative closing speed of 10 km/s:

E = ½ × m × v² = 0.5 × 0.0014 kg × (10,000 m/s)² = 71 kJ

That is the energy of a 1,000 kg car at 43 km/h, concentrated in a point the size of a fingertip. Make the sphere 10 cm and its mass grows with the cube of the radius, so the energy is 1,000 times larger: 71 MJ, about 17 kg of TNT. This is why the line between shielding and interception falls near 10 cm.

Go deeper: The layered defence Design value

Two defence sites sit forward, at about 9,700 m along the axis, and two aft, at about −9,500 m. The layers run from long range to short: detection and tracking, cargo capture far from the station, heavy interceptors for large objects, rapid interceptors, then point defence close in. Civilian mass drivers share no hardware with them.

Sources and further reading

Real-world sources

  • NASA Office of the Chief Health and Medical Officer, "Design for Ionizing Radiation Protection", NASA-STD-3001 Technical Brief OCHMO-TB-020 Rev G, June 2025: nasa.gov PDF. Source of the GCR and storm descriptions, the 7 percent, 5 to 20 g/cm², 20 g/cm², 10 cm and 20 cm water figures, and the 600 and 250 millisievert limits.
  • Richard D. Johnson and Charles Holbrow (eds.), Space Settlements: A Design Study, NASA SP-413, 1977: ntrs.nasa.gov/citations/19770014162. The 0.5 rem a year population target is in the design basis chapter: nss.org/settlement/nasa/75SummerStudy/Chapt3.html.
  • NASA Orbital Debris Program Office, "Frequently Asked Questions": orbitaldebris.jsc.nasa.gov/faq. Tracking above 10 cm, about 500,000 untracked objects of 1 to 10 cm, and ISS protection up to 1 cm.
  • National Research Council, Protecting the Space Station from Meteoroids and Orbital Debris, 1997, chapter 4, "Shielding the International Space Station": nationalacademies.org/read/5532/chapter/6. The bumper concept and the 1 cm design threat.

Concordia design documents

  • Concordia engineering specification, sections 4, 6, 7 and 43, and the exterior defence design note.