What the machine is made of, the neutron environment those materials live in, and the safety and environmental case that follows — stated with conditions, not slogans.
Solve the blanket, live
neutronics · live
Change Li-6 enrichment, thickness, multiplier and coverage and watch net TBR recompute on the deposited engine — the surrogate OpenMC retires. Request the full Monte-Carlo run to HPC.
The materials, neutronics, activation and exhaust engineering behind Hyperion — with the hard problems (first-wall dpa, divertor radiative fraction) shown as plainly as the strengths.
Superconducting Magnets · REBCO
Peak field
16.84 T on-conductor
≤ 20.1 T limit
3.3 T margin to the [HAR23] conductor limit.
REBCO neutron lifetime
OPEN
the lab-free risk
Jc degrades above a fast-neutron fluence — the one risk lab magnets never face.
Advanced Structural & Conductor Materials
Conductor substrate
MP35N S_y ~1.7 GPa
Ni-Co superalloy
High-strength substrate carrying the winding-pack Lorentz load at 4.5 K.
Preload system
~2 GPa (ice-piston)
strain 0.233%
Water→20 K expansion preloads the pack, offsetting Lorentz stress; keeps REBCO strain under 0.4%.
Vessel candidate
CrMoNbV HEA
reduced-activation
High-entropy-alloy vessel candidate — strength plus reduced activation (development-stage).
High-temp armour
HfC / TaC ~4200 K
ultra-refractory
Ultra-high-temperature ceramics for the highest-flux armour zones.
Grounded in the 16-track REBCO magnet study + tape-conductor program. Every value carries its basis tag: SOURCED / PUBLIC-DATA, DESIGN-ASSUMPTION, REQUIREMENT, or REFUTED / INFEASIBLE.
Field ladder — plug requirement vs. demonstrated coils
REQUIREMENT + PUBLIC
Plug throat — REQUIREMENT (lower)
26.49 T
Plug throat — REQUIREMENT (upper)
39.74 T
WHAM HTS mirror (CFS, as-built)
17 T
SPARC TFMC (coil test, no plasma)
20.1 T
Frank/Realta end-plug (design study)
25 T
NHMFL all-SC DC record
32.35 T
Hahn "Little Big Coil" (conductor bound)
45.5 T
The plug field is a requirement pair, 26.49–39.74 T (never quote the lower alone). It sits above today's as-built fusion magnets (WHAM 17 T, SPARC TFMC 20.1 T) but within the envelope of record all-superconducting coils (32.35 T) and demonstrated conductor capability (45.5 T). Bore/radial build for the plug is a design assumption, not sourced.
REBCO tape — critical current J_c(B) at 4.2 K
PUBLIC-DATA
B = 5 T
17.59 MA/cm²
B = 10 T
10.83 MA/cm²
B = 15 T
8.15 MA/cm²
B = 20 T
6.66 MA/cm²
Superconductor-layer J_c from public tape data (power-law B-scaling from a 20 T anchor, 50 µm Cu / 1.5 µm REBCO in 100 µm tape). Current density falls with field — the plug operates deep on this curve, which is why the winding-pack cross-section (below) matters so much.
Winding-pack cross-section (λ breakdown)
SOURCED
REBCO (superconductor)
1.34 % carries all J_c
Silver overlayer
1.34 % cap / current-share
Copper stabilizer (2×20 µm)
26.81 % quench protection
Hastelloy C-276 substrate
33.51 % tape backbone (σ_y~1.2 GPa)
Buffer stack
0.13 % ~negligible area
MP35N co-wind
33.51 % structural reinforcement (σ_y~2 GPa)
Turn insulation
3.35 % thin oxide / polyimide
The superconductor is only 1.34% of the cross-section; two-thirds is structure (Hastelloy + MP35N co-wind) carrying the hoop load. This is why the magnet is a structural problem, not just a superconductor one.
Structural materials
SOURCED-CRYO + DESIGN
Material
Property
Value
T
MP35N (cold-rolled+aged)
0.2% yield
2500 MPa
77 K
MP35N
design allowable (this study)
2000 MPa
20 K
MP35N
Young's modulus
230 GPa
77 K
Hastelloy C-276
substrate yield
~1200 MPa
cryo
Carbon-fiber overband
tensile (fiber dir.)
2000 MPa
77 K
Carbon-fiber overband
modulus (fiber dir.)
150 GPa
77 K
Bore-resolved static stress @ 26.49 T — refutes the field-only scaling
COMPUTED vs REFUTED
bore 0.02 m
87.4 MPa
bore 0.03 m
131.1 MPa
bore 0.05 m
218.5 MPa
bore 0.07 m
306 MPa
bore 0.08 m
349.7 MPa
Bore-resolved hoop stress (87–350 MPa across the swept bore) sits well under the reinforced allowable (1091 MPa) and the MP35N single-material allowable (2000 MPa). This refutes the naïve field-only scaling that predicted ~1047 MPa and looked marginal. Static structure is feasible; the binding problem is cyclic (next).
Cyclic fatigue at operating field — the binding gate
INFEASIBLE
Case
σ_max
N to failure
Design cycles
Verdict
26.49 T, no preload
3289 MPa
2.3×10⁻³
10,000
INFEASIBLE
26.49 T, engineered preload
2916 MPa
9.3×10⁻²
10,000
INFEASIBLE
39.74 T, engineered preload
3881 MPa
3.9×10⁻⁵
10,000
INFEASIBLE
Layer-resolved FEA hoop stress at operating field exceeds the fatigue allowable — the coil would not survive its cycle count. This is stated as a gate, not a solved result: it needs a full bore-resolved winding-pack FEA and a fatigue-qualified reinforcement/preload scheme. It is the #1 magnet open item on the Open Risks ↗ page.
Magnet neutron lifetime vs. tungsten shield
DESIGN-STUDY
no shield
0.023 FPY
5 cm W
0.067 FPY
10 cm W
0.194 FPY
12.5 cm W
0.33 FPY
15 cm W
0.562 FPY
Even at 15 cm of tungsten the magnet reaches only ~0.56 full-power-years — below the 2 FPY replacement target (gold line = target). Shield optimisation and advanced-pinning (APC) conductor are needed; confirm with neutron-transport (MCNP) runs. An open lifetime item.
Quench protection
SELF-PROTECTING
Case
Stored E
T_max
V_terminal
Self-protecting
26.49 T
2.35 MJ
145 K
405 V
YES
39.74 T
39.4 MJ
109 K
455 V
YES
The VOx metal-insulation approach is self-protecting (peak temperatures well below damage limits), benchmarked against Suetomi 2021 (model reproduces the 330 K reference). Good news among the harder magnet items.
Materials qualification — where each stands
HONEST STATUS
Item
Status
Note
REBCO tape
Commercial
J_c well-characterised; fusion-fluence lifetime open
MP35N reinforcement
Qualified (cryo)
Cryogenic yield sourced
Hastelloy C-276
Commercial
Standard tape substrate
Tungsten PFC / shield
Established
PFC-grade W; shield thickness to be optimised
Plug winding-pack (fatigue)
NOT qualified — GATE
Needs bore-resolved FEA + fatigue design
Neutron shield adequacy
Design study
MCNP confirmation pending
Breeder deposit · DOI 10.5281/zenodo.21746157 · reproduced from the open Zenodo/GitHub deposit (CC BY 4.0). Canonical freeze: FROZEN_2026-08_PUBLICATION.csv. · Materials/neutronics screening; UNCOMPUTED terms named, not estimated.
🔒 Materials & Neutronics is Kronos-only. The overview above is public — the full data, tables, live calculations and engineering detail on this page require a Kronos team sign-in.
Safety case · Breeder · Hyperion
Safety Case
Preliminary hazard analysis for the frozen design — failure modes (FMEA), process deviations (HAZOP) and the radiological picture (activation, decay heat, waste). Fusion's inherent safety is the backdrop: no chain reaction, no criticality, no meltdown path, and decay heat orders of magnitude below fission.
⚠ Preliminary — screening level. This is a design-stage hazard analysis, not a licensed safety case. FMEA/HAZOP entries are representative and await a full facilitated study; the activation inventory awaits a FISPACT-II run. It states the hazards honestly rather than asserting compliance.
Criticality risk
NONE
no chain reaction · no meltdown path
FMEA items
6
0 at RPN ≥ 100
Decay heat vs fission
≪ 1%
vs ~7% · passively removable
Waste class
Class C LLW
no HLW · no actinides
FMEA — failure modes & effects
RPN = Severity × Occurrence × Detection (1–10 each) · higher = more risk · click a row for detail
Item
Failure mode
Effect
S
O
D
RPN
Requirement
TF magnet
Quench
Field loss → plasma benignly terminates; possible coil damage
7
3
4
84
REQ-B09 ↗
Plasma
Major disruption
EM + thermal transient on first wall & vessel
6
4
4
96
REQ-B08 ↗
Divertor coolant
Loss of flow
Target overheating → PFC erosion
6
3
3
54
REQ-B07 ↗
Tritium plant
Containment breach
Tritium release — radiological
8
2
5
80
REQ-B02 ↗
Vacuum vessel
Air ingress
Plasma disrupts (benign) + oxidation risk
5
2
3
30
REQ-B08 ↗
Cryoplant
Helium release
Oxygen-deficiency (ODH) in the hall
6
2
4
48
—
HAZOP — guideword deviations
Guideword
Parameter
Cause
Consequence
Safeguard
NO
Coolant flow
Pump trip / blockage
PFC & first-wall overheat
Interlock trip + passive cooling loop
MORE
Coolant pressure
Blockage / thermal transient
Pipe rupture
Relief valves + design pressure rating
LESS
Chamber vacuum
Leak / seal failure
Plasma disruption (benign)
Fast shutdown + isolation valves
MORE
Magnet temperature
Cooling loss
Quench
Detection + stored-energy dump
AS WELL AS
Tritium in coolant
Permeation
Secondary contamination
Detritiation loop + monitoring
MORE
Plasma density
Control fault
Disruption
Density-limit control + mitigation valves
Radiological — activation, decay heat & waste
Dominant hazard
Tritium
on-site inventory · multi-barrier
Activated structure
RAFM steel
Class C LLW · recyclable ~100 yr
Long-lived actinides
NONE
not a fission fuel cycle
Neutron wall load
1.97 MW/m²
14 MeV D–T dominated
Decay heat after shutdown representative
Radiological picture
Criticality / meltdownnot physically possible
Decay heat at shutdown~1% of P_fus (fission ~7%)
Passive heat removalsufficient — no active cooling needed to stay safe
FISPACT-II nuclide inventoryUNCOMPUTED — needs the activation run
The breeder concentrates the radiological burden at one isolatable, remotely-sited machine — tritium handling is the design-driving hazard, addressed by multiple confinement barriers.
Preliminary hazard analysis over the frozen design · decay-heat curve is representative (needs a FISPACT-II / decay-heat run) · FMEA & HAZOP await a facilitated study. PRELIMINARY · NOT A LICENSED SAFETY CASE
🔒 Safety Case is Kronos-only. The overview above is public — the full data, tables, live calculations and engineering detail on this page require a Kronos team sign-in.
Environmental · screening-level LCA (ISO 14040/44)
Environmental Profile
A comparative, honest life-cycle assessment of the two-machine fleet against the technologies it displaces and against other fusion cycles. Screening-grade where noted; terms not yet computed are named, not estimated.
Lifecycle carbon · gCO₂eq/kWh (IPCC AR5 WG3)
Coal820 g
Natural gas490 g
Biomass230 g
Solar PV48 g
Hydro24 g
Nuclear12 g
Wind onshore11 g
Kronos burner12 g
— operational only~0 op
IPCC AR5 WG3 median lifecycle emissions. Fusion has no combustion → operational ~0; embodied is nuclear/wind class.
Neutron cleanliness · % of fusion energy carried by neutrons
D–T tokamak (ITER/DEMO)80 %
Kronos breeder (product)79.7 %
Kronos burner · x 0.305.44 %
Kronos burner · x 0.432.77 %
p–B¹¹ (ideal aneutronic)0.5 %
The burner is low-neutron (5.44%), not aneutronic — ~10–15× cleaner than a mainstream D–T tokamak, not as clean as ideal p–B¹¹. A free clean-shift to x 0.35 reaches 4.18% and stays net-positive. The breeder is deliberately neutron-rich — its 14 MeV neutrons are the product.
Safety · deaths per TWh (Our World in Data)
Coal
24.6
deaths/TWh
Natural gas
2.8
deaths/TWh
Nuclear
0.03
deaths/TWh
Wind / solar
~0.03
deaths/TWh
Radioactive waste
Breeder (Hyperion) ≤ Class C
with low-activation RAFM steel
RAFM Nb<10ppmSoF 0.464 (2.2× under)
RAFM Nb<1ppmSoF 0.087 (12× under)
generic 316SSGTCC — no US pathway
volume264–661 t · 34–85 m³ / 40 yr
Burner (Aegis/MetroVolt) ~ Class A
~0 scheduled activated waste
first-wall changes0.035–0.144 / 30 yr
scheduled stream~0 (negligible)
wall loading41–168× below breeder
REBCO plug coilsUNCOMPUTED
Fleet strategy · concentrate & isolate vs distribute clean
The fleet concentrates its unavoidable radiological cost at one isolatable, remotely-sited breeder, while distributing clean, low-neutron burners to the point of use. Radiological burden is centralized and contained; generation is clean and distributed — the fleet is ~10–15× cleaner in neutron terms than a mainstream D–T tokamak, and net-favourable versus the incumbents it displaces on carbon, land, waste longevity and safety.
Embodied carbon & materials
Burner
12 gCO₂eq/kWh (5–30)
nuclear/wind class; construction 60–70% of emissions
Breeder
~13 tCO₂ / kg-T
embodied screening; operational is grid-dependent (25.9 MWe draw)
Driver
steel + concrete + magnets
same finding across fusion LCA studies
Stated honestly · not yet computed
We name what we have not computed rather than estimate beyond the evidence:
Absolute D–D tritium production at commercial scaleUNCOMPUTED
Full activation curie inventory & decay heat (needs FISPACT on a certified heat)UNCOMPUTED
Embodied carbon at bill-of-materials fidelityUNCOMPUTED
Screening-level LCA (ISO 14040/44). Comparators: IPCC AR5 WG3 Annex III · Our World in Data · fusion LCA (Tokimatsu et al.). Every burner figure carries the plug-density requirement caveat.
🔒 Environmental Profile is Kronos-only. The overview above is public — the full data, tables, live calculations and engineering detail on this page require a Kronos team sign-in.
KRONOS FUSION ENERGY · Kronos ModelConceptual design and simulation study; no machine has been built