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DEMO (Demonstration Power Plant)

DEMO (DEMOnstration Power Plant) is the next-generation fusion device designed to demonstrate the technical and economic feasibility of fusion power generation. While ITER aims for scientific demonstration of fusion energy, DEMO will actually deliver electricity to the power grid, serving as a bridge to commercial fusion power plants.

Fusion research has a history of over 60 years, but no fusion device has ever produced electricity. DEMO carries the historic mission of demonstrating to the world that fusion energy can be a practical energy source.

Position Between ITER and Commercial Reactors

Section titled “Position Between ITER and Commercial Reactors”

Hierarchical Structure of Fusion Development

Section titled “Hierarchical Structure of Fusion Development”

The development toward fusion power generation progresses in stages from scientific demonstration to economic realization. Each stage builds upon the achievements of the previous one and aims to solve new technical challenges.

StageDevicePrimary ObjectiveQ ValueTarget Timeline
Experimental ReactorITERAchieve Q=10, Demonstrate Burning Plasma102035~
Prototype ReactorDEMOPower Generation Demonstration, Tritium Self-Sufficiency25-402040s-2050s
Demonstration Reactor-Economic and Reliability Demonstration40+2050s~
Commercial Reactor-Practical Power Generation40+2060s~

In the fusion field, the distinction between prototype reactor and demonstration reactor differs from fission power generation. From the perspective of fusion output, the difference between prototype and demonstration reactors is small, and since the prototype reactor often fulfills the functions of the demonstration reactor as well, they are collectively referred to as DEMO.

Several decisive technical leaps are required between ITER and DEMO.

Technology Maturity Index=f(Q value,Availability,TBR,Net Electric Output)\text{Technology Maturity Index} = f(\text{Q value}, \text{Availability}, \text{TBR}, \text{Net Electric Output})

Comparing the required specifications of ITER and DEMO reveals the magnitude of this leap.

ParameterITERDEMOLeap Factor
Fusion Power PfusP_\mathrm{fus}500 MW2000-3000 MW4-6x
Q Value1025-402.5-4x
Pulse Length400-600 secondsSteady-state or 2+ hours10x+
AvailabilityFew % (experimental device)30-50%10x+
TBR (Tritium Breeding Ratio)N/A1.05+New requirement
Net Electric OutputNone300-500 MWNew requirement

The Q value (energy multiplication factor) is defined as the ratio of fusion power to heating input:

Q=PfusPheatQ = \frac{P_\mathrm{fus}}{P_\mathrm{heat}}

ITER’s target of Q=10 is sufficient for scientific demonstration of fusion energy, but for the power generation system to be viable, the net electric output, accounting for auxiliary power and thermal losses, must be positive.

Requirements for Power Generation System Viability

Section titled “Requirements for Power Generation System Viability”

For DEMO to be viable as a power generation system, the net electric output PnetP_\mathrm{net} must be positive:

Pnet=ηthPthPauxPrecircP_\mathrm{net} = \eta_\mathrm{th} \cdot P_\mathrm{th} - P_\mathrm{aux} - P_\mathrm{recirc}

Where:

  • ηth\eta_\mathrm{th}: Thermal conversion efficiency (typically 30-40%)
  • PthP_\mathrm{th}: Thermal output (fusion power plus neutron multiplication and heating in structural materials)
  • PauxP_\mathrm{aux}: Auxiliary power (cooling systems, control systems, etc.)
  • PrecircP_\mathrm{recirc}: Recirculating power (plasma heating, current drive, etc.)

The relationship between fusion power PfusP_\mathrm{fus} and thermal output PthP_\mathrm{th} is:

Pth=Pfus×MP_\mathrm{th} = P_\mathrm{fus} \times M

Here, MM is the energy multiplication factor, typically around 1.1-1.3 due to neutron multiplication reactions in the blanket.

The recirculating power fraction frecircf_\mathrm{recirc} is an important indicator of power generation efficiency:

frecirc=PrecircPgrossf_\mathrm{recirc} = \frac{P_\mathrm{recirc}}{P_\mathrm{gross}}

For commercial reactor viability, frecirc<0.2f_\mathrm{recirc} < 0.2 is desirable, which is the primary reason for requiring high-Q operation.

As a “prototype” of commercial reactors, DEMO must demonstrate the following functions:

  1. Achievement of net electric output (hundreds of MW class)
  2. Tritium fuel self-sufficiency
  3. High availability operation (30% or more)
  4. Component replacement through remote maintenance
  5. Demonstration of licensable safety

These functional demonstrations will establish the technological foundation for commercial reactor design.

Multiple countries and regions, centered on ITER participants, are advancing their own DEMO plans. Each plan has distinctive characteristics in terms of technical approach and development schedule.

The European DEMO plan led by EUROfusion is the world’s most systematically advanced prototype reactor development program. Conceptual studies progressed under Horizon 2020 starting in 2014, and the formal Pre-Conceptual Design Phase began in 2021. Conceptual design is scheduled for completion by 2027, with operation start targeted for 2051.

EUROfusion is a consortium of fusion research institutions from over 30 European countries, advancing DEMO development with an annual budget of approximately 600 million euros.

EU-DEMO’s design parameters are set from the perspective of balancing power generation demonstration and technology transfer to commercial reactors.

ParameterValueNotes
Major Radius R0R_09.0 m1.45x ITER (6.2m)
Minor Radius aa2.9 m
Aspect Ratio A=R0/aA = R_0/a3.1
Plasma Current IpI_p18-20 MA
Toroidal Field BTB_T5.7-5.9 T (on-axis)
Fusion Power PfusP_\mathrm{fus}2000 MW
Q Value40-50
Net Electric Output PnetP_\mathrm{net}300-500 MW
Thermal Conversion Efficiency33-36%
TBR> 1.05
Pulse Length2+ hoursSteady-state operation also in view

Plasma performance is characterized by normalized beta βN\beta_N and Greenwald density fraction n/nGn/n_G:

βN=βIp/(aBT)×1002.53.0\beta_N = \frac{\beta}{I_p/(aB_T)} \times 100 \approx 2.5-3.0 nnG0.81.0\frac{n}{n_G} \approx 0.8-1.0

The Greenwald density limit is:

nG=Ipπa2×1020m3n_G = \frac{I_p}{\pi a^2} \times 10^{20} \, \mathrm{m}^{-3}

Two blanket concepts are being studied in parallel for EU-DEMO.

Helium Cooled Pebble Bed (HCPB):

  • Breeder: Lithium ceramic (Li₄SiO₄ or Li₂TiO₃) pebbles
  • Multiplier: Beryllium pebbles
  • Coolant: High-pressure helium (8 MPa, inlet 300°C / outlet 500°C)
  • Structural material: EUROFER97 (reduced activation ferritic steel)

Water Cooled Lithium Lead (WCLL):

  • Breeder/Multiplier: Liquid lithium-lead (Pb-15.7Li)
  • Coolant: Pressurized water (15.5 MPa, inlet 295°C / outlet 328°C)
  • Structural material: EUROFER97

TBR evaluation for both concepts is performed by Monte Carlo neutron transport calculations:

TBR=σ6Li(n,α)tϕnN6LidV+σ7Li(n,nα)tϕnN7LidV\mathrm{TBR} = \int \sigma_{\mathrm{^6Li}(n,\alpha)t} \cdot \phi_n \cdot N_{\mathrm{^6Li}} \, dV + \int \sigma_{\mathrm{^7Li}(n,n'\alpha)t} \cdot \phi_n \cdot N_{\mathrm{^7Li}} \, dV

Here, σ\sigma is the reaction cross-section, ϕn\phi_n is the neutron flux, and NN is the nuclide density.

EU-DEMO’s divertor heat load will be more severe than ITER:

qdiv=PSOLAwet1020MW/m2q_\mathrm{div} = \frac{P_\mathrm{SOL}}{A_\mathrm{wet}} \approx 10-20 \, \mathrm{MW/m^2}

Here, PSOLP_\mathrm{SOL} is the heat flux to the scrape-off layer, and AwetA_\mathrm{wet} is the wetted area of the divertor.

The scrape-off layer width λq\lambda_q is estimated by Eich scaling:

λqBpol1.19\lambda_q \propto B_\mathrm{pol}^{-1.19}

For EU-DEMO, the following divertor concepts are being studied:

  • Water-cooled tungsten single-null (extension of ITER type)
  • Liquid metal divertor (tin or lithium)
  • Advanced divertor configurations (Super-X, Snowflake)

Japan’s prototype reactor plan is centered on the National Institutes for Quantum Science and Technology (QST) and the National Institute for Fusion Science (NIFS), utilizing the results of BA (Broader Approach) activities conducted in parallel with ITER.

In 2019, the basic concept was clarified by the Ministry of Education, Culture, Sports, Science and Technology’s Prototype Reactor Development Comprehensive Strategy Task Force. In April 2023, the Cabinet Office formulated the “Fusion Energy Innovation Strategy.” Under this strategy, efforts toward power generation demonstration in the 2030s are accelerating.

JA-DEMO is based on a design philosophy emphasizing steady-state operation.

ParameterValueNotes
Major Radius R0R_08.5 m
Minor Radius aa2.4 m
Aspect Ratio AA3.5Higher than EU-DEMO
Plasma Current IpI_p12.3 MASuppressed for steady-state operation
Toroidal Field BTB_T6.0 T (on-axis)
Fusion Power PfusP_\mathrm{fus}1500 MW
Q Value25-40
Gross Electric Output640 MW
Net Electric Output300 MW
TBR> 1.05
Operating ModeSteady-state or 2-hour pulses

A distinctive feature of JA-DEMO is the pursuit of high bootstrap current fraction fBSf_\mathrm{BS}:

fBS=IBSIp0.70.8f_\mathrm{BS} = \frac{I_\mathrm{BS}}{I_p} \approx 0.7-0.8

The bootstrap current is a current spontaneously driven by pressure gradients:

IBS1BθprI_\mathrm{BS} \propto -\frac{1}{B_\theta} \frac{\partial p}{\partial r}

High fBSf_\mathrm{BS} reduces the burden of external current drive and lowers recirculating power.

JA-DEMO development is closely coordinated with the following BA activity facilities:

JT-60SA (Superconducting Tokamak):

  • Demonstration of steady-state high-beta plasma
  • Development of advanced operating scenarios
  • Establishment of disruption mitigation techniques

IFMIF-DONES (Fusion Neutron Source):

  • Irradiation testing of DEMO materials
  • Damage evaluation by fast neutrons (14 MeV)
  • Accelerated irradiation of 20-50 dpa per year

IFERC (International Fusion Energy Research Centre):

  • Coordination of DEMO design activities
  • Simulations using supercomputers
  • Development of remote experimentation technology

JA-DEMO milestones:

  • Around 2025: Transition to engineering design
  • 2027: JT-60SA deuterium experiments begin
  • Early 2030s: Construction start decision
  • 2035: ITER burning experiments begin (data acquisition)
  • Mid-2040s: Operation start

An advancement of about 5 years from the original target of around 2050 is being considered.

The China Fusion Engineering Test Reactor (CFETR) is China’s own plan aiming to bridge ITER and commercial reactors. Led by the Institute of Plasma Physics, Chinese Academy of Sciences (ASIPP), conceptual design was completed in 2017 and engineering design in 2020.

China has the world’s largest number of fusion researchers (approximately 3,000) and is channeling technology accumulated from predecessor devices such as EAST and HL-2M into CFETR.

CFETR is characterized by a two-phase operation plan.

ParameterPhase IPhase II
Major Radius R0R_07.2 m7.2 m
Minor Radius aa2.2 m2.2 m
Aspect Ratio AA3.33.3
Plasma Current IpI_p10 MA14 MA
Toroidal Field BTB_T6.5 T6.5 T
Fusion Power PfusP_\mathrm{fus}50-200 MW1000+ MW
Q Value1-510+
TBR> 1.0> 1.2

Phase I focuses on engineering testing and technology demonstration, with full-scale power generation demonstration in Phase II.

Prior to CFETR, technology development is progressing at the following facilities:

CRAFT (Comprehensive Research Facilities for Fusion Technology):

  • Superconducting magnet fabrication and testing
  • Divertor heat load testing
  • Blanket technology development
  • Location: Hefei

BEST (Burning plasma Experimental Superconducting Tokamak):

  • Spherical tokamak configuration
  • Expected completion in 2027
  • Research on high-beta plasma
  • Open to international collaboration

CFETR milestones:

  • 2017: Conceptual design completed
  • 2020: Engineering design completed
  • Late 2020s to around 2030: Construction start
  • Mid-2030s: Phase I operation start
  • 2040s: Phase II operation start

South Korea is planning K-DEMO based on achievements from KSTAR (Korea Superconducting Tokamak Advanced Research). In 2024, the “Accelerated Fusion Energy Realization Strategy” was announced, with clarification of the development schedule and significant budget increases.

This strategy also added the construction of CPD (Compact Pilot Device) as an intermediate step prior to K-DEMO.

ParameterK-DEMONotes
Major Radius R0R_06.8 m
Minor Radius aa2.1 m
Aspect Ratio AA3.2
Plasma Current IpI_p12 MA
Toroidal Field BTB_T7.4 THTS adoption
Fusion Power PfusP_\mathrm{fus}2200 MW
Net Electric Output500 MW
TBR> 1.05

A distinctive feature of K-DEMO is the design based on the adoption of High-Temperature Superconducting (HTS) coils. HTS enables higher magnetic fields, and device compactness and improved economics are expected.

CPD is planned as an intermediate step prior to K-DEMO:

ParameterCPD
Major Radius R0R_04.5-5.0 m
Fusion Power PfusP_\mathrm{fus}200-400 MW
ObjectiveSteady-state operation technology demonstration
Operation StartEarly 2040s

K-DEMO milestones:

  • 2030s: CPD construction and operation
  • 2040s: K-DEMO construction start
  • After 2050: K-DEMO operation start

International Comparison of Design Parameters

Section titled “International Comparison of Design Parameters”

A unified comparison of DEMO plans from each region.

ParameterEU-DEMOJA-DEMOCFETR-IIK-DEMO
Major Radius R0R_0 [m]9.08.57.26.8
Minor Radius aa [m]2.92.42.22.1
Aspect Ratio AA3.13.53.33.2
Plasma Current IpI_p [MA]18-2012.31412
Toroidal Field BTB_T [T]5.7-5.96.06.57.4
Fusion Power PfusP_\mathrm{fus} [MW]2000150010002200
Q Value40-5025-401030-40
Net Electric Output [MW]300-500300-500
Operation Start Target205120452035-40After 2050

For comparing plasma performance, the fusion triple product is useful:

niTiτE3×1021keVsm3n_i T_i \tau_E \geq 3 \times 10^{21} \, \mathrm{keV \cdot s \cdot m^{-3}}

Triple product margin in each DEMO design:

Mignition=(niTiτE)design(niTiτE)LawsonM_\mathrm{ignition} = \frac{(n_i T_i \tau_E)_\mathrm{design}}{(n_i T_i \tau_E)_\mathrm{Lawson}}

Realizing DEMO requires solving technical challenges that cannot be sufficiently verified in ITER. These challenges are interrelated, and integrated solutions are required.

The D-T fusion reaction consumes tritium (T) as fuel:

D+Tα(3.5MeV)+n(14.1MeV)\mathrm{D} + \mathrm{T} \rightarrow \alpha (3.5 \, \mathrm{MeV}) + n (14.1 \, \mathrm{MeV})

The tritium consumption rate is proportional to fusion power:

m˙T=Pfus17.6MeV×mT55.8kg/GWyear\dot{m}_T = \frac{P_\mathrm{fus}}{17.6 \, \mathrm{MeV}} \times m_T \approx 55.8 \, \mathrm{kg/GW \cdot year}

A fusion power of 1 GW consumes approximately 56 kg of tritium per year.

However, tritium is a radioactive isotope with a half-life of 12.3 years and exists only in trace amounts in nature. Current world supply is about 25 kg (mainly recovered from Canadian CANDU reactors), and tritium production (breeding) within the reactor is essential to sustain fusion power generation beyond DEMO.

Tritium production in the blanket is achieved through nuclear reactions between lithium and neutrons:

6Li+nT+α+4.78MeV\mathrm{^6Li} + n \rightarrow \mathrm{T} + \alpha + 4.78 \, \mathrm{MeV} 7Li+nT+α+n2.47MeV\mathrm{^7Li} + n \rightarrow \mathrm{T} + \alpha + n' - 2.47 \, \mathrm{MeV}

The ⁶Li reaction is highly efficient with thermal neutrons, while the ⁷Li reaction requires fast neutrons and is endothermic.

The Tritium Breeding Ratio (TBR) is:

TBR=Tritium producedTritium consumed\mathrm{TBR} = \frac{\text{Tritium produced}}{\text{Tritium consumed}}

DEMO requires TBR > 1.05. This margin compensates for the following losses:

  • Tritium decay losses (half-life 12.3 years)
  • Losses during fuel cycle (recovery efficiency < 100%)
  • Accumulation as startup inventory
  • Supply to new reactors

The following design innovations are needed to increase TBR:

Use of neutron multiplier materials:

Be+n2n+Be\mathrm{Be} + n \rightarrow 2n + \mathrm{Be^*} Pb+n2n+Pb\mathrm{Pb} + n \rightarrow 2n + \mathrm{Pb^*}

By using beryllium or lead as multiplier materials, multiple neutrons can be generated from a single 14.1 MeV neutron, increasing tritium production reactions.

⁶Li enrichment: Natural lithium has a composition of 7.5% ⁶Li and 92.5% ⁷Li, but TBR can be improved by enriching ⁶Li (30-90%).

Blanket coverage: Minimizing neutron leakage through ports and gaps is also important. If the coverage fraction is fcovf_\mathrm{cov}:

TBRactualTBRideal×fcov\mathrm{TBR_{actual}} \approx \mathrm{TBR_{ideal}} \times f_\mathrm{cov}

Typically fcov0.850.90f_\mathrm{cov} \approx 0.85-0.90, resulting in a 10-15% reduction from ideal TBR.

DEMO’s tritium fuel cycle consists of the following subsystems:

  1. Fuel supply system: Fuel injection by pellet injection or gas puff
  2. Exhaust processing system: Exhaust gas processing from divertor
  3. Isotope separation system: Separation and purification of H/D/T
  4. Tritium recovery system: Tritium extraction from blanket
  5. Storage and accounting system: Tritium inventory management
  6. Confinement and safety system: Confinement by multiple barriers

Burn fraction ηb\eta_b (burn rate relative to injected fuel) is typically low at 1-5%:

ηb=T burnedT injected0.010.05\eta_b = \frac{\text{T burned}}{\text{T injected}} \approx 0.01-0.05

Unburned tritium is recovered and reused, but this low burn fraction increases tritium inventory.

For a fusion reactor to be viable as a power generation system, a sufficiently high Q value is necessary.

The main components of recirculating power PrecircP_\mathrm{recirc} are:

Precirc=Pheat+PCD+Pcryo+PpumpP_\mathrm{recirc} = P_\mathrm{heat} + P_\mathrm{CD} + P_\mathrm{cryo} + P_\mathrm{pump}

Where:

  • PheatP_\mathrm{heat}: Plasma heating power
  • PCDP_\mathrm{CD}: Current drive power
  • PcryoP_\mathrm{cryo}: Cryogenic refrigeration power
  • PpumpP_\mathrm{pump}: Vacuum and cooling pump power

Net electric output is:

Pnet=ηthMPfusPrecircP_\mathrm{net} = \eta_\mathrm{th} M P_\mathrm{fus} - P_\mathrm{recirc}

The relationship between Q value and net electric output is:

Pnet=Pfus(ηthMηCD1(1fBS)QPotherPfus)P_\mathrm{net} = P_\mathrm{fus} \left( \eta_\mathrm{th} M - \frac{\eta_\mathrm{CD}^{-1}(1-f_\mathrm{BS})}{Q} - \frac{P_\mathrm{other}}{P_\mathrm{fus}} \right)

Here, ηCD\eta_\mathrm{CD} is current drive efficiency, fBSf_\mathrm{BS} is bootstrap current fraction, and PotherP_\mathrm{other} is auxiliary power other than heating.

The minimum required Q value is derived from the condition Pnet>0P_\mathrm{net} > 0. For typical DEMO parameters, Q > 20-30 is required.

Achieving high-Q operation requires the following plasma conditions:

Fusion power density:

pfus=EfusnDnTσvDTp_\mathrm{fus} = E_\mathrm{fus} \cdot n_D n_T \langle \sigma v \rangle_{DT}

Here, σvDT\langle \sigma v \rangle_{DT} is the D-T reaction rate, which is a function of temperature TT:

σvDT1.1×1024T2m3/s(10T20keV)\langle \sigma v \rangle_{DT} \approx 1.1 \times 10^{-24} T^2 \, \mathrm{m^3/s} \quad (10 \lesssim T \lesssim 20 \, \mathrm{keV})

Fusion power scales as:

Pfusβ2B4R3/A4P_\mathrm{fus} \propto \beta^2 B^4 R^3 / A^4

Here, β\beta is the beta value (ratio of plasma pressure to magnetic pressure):

β=2μ0pB2\beta = \frac{2\mu_0 \langle p \rangle}{B^2}

High beta and high magnetic field are advantageous for high Q, but are constrained by MHD stability limits and coil technology.

Toroidal beta βt\beta_t is constrained by the Troyon limit:

βt[%]βNIp[MA]a[m]BT[T]\beta_t [\%] \leq \beta_N \frac{I_p [\mathrm{MA}]}{a [\mathrm{m}] B_T [\mathrm{T}]}

The limit value of normalized beta βN\beta_N is approximately 2.8 in ideal MHD, but 3.5 or higher is possible with resistive wall mode (RWM) stabilization.

DEMO requires stable operation at βN2.53.0\beta_N \approx 2.5-3.0.

In the tokamak configuration, pulsed operation is fundamental because plasma current is induced by transformer principles.

The magnetic flux consumption rate is:

dΨdt=Vloop=RpIp+LpdIpdt\frac{d\Psi}{dt} = V_\mathrm{loop} = R_p I_p + L_p \frac{dI_p}{dt}

In steady state (dIp/dt=0dI_p/dt = 0):

Vloop=RpIp=ηJpneTe3/2IpV_\mathrm{loop} = R_p I_p = \frac{\eta_\parallel J_p}{n_e T_e^{3/2}} I_p

To maintain steady-state operation, plasma current must be sustained by non-inductive means (non-inductive current drive).

Bootstrap current is a current spontaneously driven by pressure gradients:

jBS=pBθdpdrL31j_\mathrm{BS} = -\frac{p}{\langle B_\theta \rangle} \frac{dp}{dr} L_{31}

Here, L31L_{31} is the neoclassical transport coefficient.

The bootstrap current fraction is:

fBS=IBSIpϵβpf_\mathrm{BS} = \frac{I_\mathrm{BS}}{I_p} \propto \sqrt{\epsilon} \beta_p

Here, ϵ=a/R0\epsilon = a/R_0 is the inverse aspect ratio and βp\beta_p is the poloidal beta.

Achieving high fBSf_\mathrm{BS} (0.7-0.8) can significantly reduce the burden of external current drive.

The remaining current (1fBS1 - f_\mathrm{BS}) is maintained by external current drive:

Neutral Beam Injection (NBI) current drive:

ηNBI=ne,20RICDPNBI0.20.4×1020A/(Wm2)\eta_\mathrm{NBI} = \frac{n_{e,20} R I_\mathrm{CD}}{P_\mathrm{NBI}} \approx 0.2-0.4 \times 10^{20} \, \mathrm{A/(W \cdot m^2)}

Radio-frequency current drive (ECCD/LHCD):

ηECCD0.20.3×1020A/(Wm2)\eta_\mathrm{ECCD} \approx 0.2-0.3 \times 10^{20} \, \mathrm{A/(W \cdot m^2)} ηLHCD0.30.5×1020A/(Wm2)\eta_\mathrm{LHCD} \approx 0.3-0.5 \times 10^{20} \, \mathrm{A/(W \cdot m^2)}

Current drive efficiency depends on density and temperature:

ηCDTene\eta_\mathrm{CD} \propto \frac{T_e}{n_e}

Efficiency improves at high temperature and low density plasma, but there is a trade-off with fusion power.

In steady-state operation, the balance between fusion power and losses is critical:

dWdt=Pα+PheatPloss\frac{dW}{dt} = P_\alpha + P_\mathrm{heat} - P_\mathrm{loss}

Here, WW is plasma stored energy, PαP_\alpha is alpha particle heating, and PlossP_\mathrm{loss} is transport loss.

In steady state (dW/dt=0dW/dt = 0):

Pα+Pheat=Ploss=WτEP_\alpha + P_\mathrm{heat} = P_\mathrm{loss} = \frac{W}{\tau_E}

In burning plasma, PαPheatP_\alpha \gg P_\mathrm{heat}, and control of alpha particle heating is key to thermal stability.

The thermal instability growth rate is:

γthermal=1τE(PαTPlossT)TP\gamma_\mathrm{thermal} = \frac{1}{\tau_E} \left( \frac{\partial P_\alpha}{\partial T} - \frac{\partial P_\mathrm{loss}}{\partial T} \right) \frac{T}{P}

Under the condition Pα/T>Ploss/T\partial P_\alpha / \partial T > \partial P_\mathrm{loss} / \partial T, thermal runaway can occur, requiring stabilization through heating control or profile control.

Definition and Requirements of Availability

Section titled “Definition and Requirements of Availability”

Availability is an important parameter that determines the economics of a fusion reactor:

favail=toptop+tmaintf_\mathrm{avail} = \frac{t_\mathrm{op}}{t_\mathrm{op} + t_\mathrm{maint}}

Here, topt_\mathrm{op} is operation time and tmaintt_\mathrm{maint} is maintenance time.

Commercial reactors require favail0.75f_\mathrm{avail} \geq 0.75 (9+ months of operation per year). DEMO targets favail0.30.5f_\mathrm{avail} \approx 0.3-0.5.

After D-T operation, the vacuum vessel interior is subject to strong activation:

D˙104106Sv/h\dot{D} \approx 10^4-10^6 \, \mathrm{Sv/h}

At this dose rate, maintenance by humans is impossible, and all in-vessel components must be replaced and maintained by remote operation.

Blanket replacement time estimate:

  • Number of segments: 100-200
  • Replacement time per segment: 10-20 hours
  • Total replacement time: Several months to 1 year

Reducing this maintenance time is key to achieving high availability.

The following maintenance scenarios are being studied for DEMO:

Horizontal port maintenance (EU-DEMO):

  • Extract blanket segments through large equatorial ports
  • Number of ports: Approximately 16
  • Segments are refurbished at factory before reinstallation

Vertical maintenance (JA-DEMO):

  • Lift entire blanket from upper ports
  • Uses large cranes and hot cells
  • High work efficiency due to large replacement units, but requires large-scale facilities

Sector maintenance:

  • Replace vacuum vessel sector by sector
  • Enables shortest shutdown time
  • Cost of spare sector manufacturing is a challenge

Improving equipment reliability is also important for achieving high availability:

Relationship between Mean Time Between Failures (MTBF) and Mean Time To Repair (MTTR):

favail=MTBFMTBF+MTTRf_\mathrm{avail} = \frac{\mathrm{MTBF}}{\mathrm{MTBF} + \mathrm{MTTR}}

For systems consisting of multiple independent components:

favail,system=ifavail,if_\mathrm{avail,system} = \prod_i f_\mathrm{avail,i}

Since fusion reactors consist of thousands of components, high reliability of each element is essential.

The divertor is the component subject to the most severe heat load in a fusion reactor:

qdiv=PSOL2πRdivλqfexpq_\mathrm{div} = \frac{P_\mathrm{SOL}}{2\pi R_\mathrm{div} \cdot \lambda_q \cdot f_\mathrm{exp}}

Where:

  • PSOLP_\mathrm{SOL}: Heat flux to scrape-off layer (approximately 20% of fusion power)
  • RdivR_\mathrm{div}: Divertor radius
  • λq\lambda_q: SOL width (a few mm)
  • fexpf_\mathrm{exp}: Magnetic flux expansion factor

At DEMO scale, qdivq_\mathrm{div} can easily reach tens to 100 MW/m², which no material can withstand.

Detachment operation: Impurities (N, Ne, Ar, etc.) are injected into the divertor region to increase radiation losses:

Prad=nenZLZ(Te)P_\mathrm{rad} = n_e n_Z L_Z(T_e)

Here, LZ(Te)L_Z(T_e) is the radiative loss coefficient.

Radiation losses disperse heat flux and reduce direct heat load to the divertor:

frad=PradPSOL0.80.9f_\mathrm{rad} = \frac{P_\mathrm{rad}}{P_\mathrm{SOL}} \gtrsim 0.8-0.9

Advanced divertor configurations:

  • Super-X divertor: Extends strike point outward to increase fexpf_\mathrm{exp}
  • Snowflake divertor: Forms additional null points near the X-point
  • X-divertor: Maximizes field line expansion

Liquid metal divertor:

  • Uses liquid surface of lithium or tin
  • Cooling by latent heat of vaporization
  • Self-healing capability
  • Reduced hydrogen recycling

In DEMO, materials are exposed to neutron fluence far exceeding ITER:

Displacement damage (dpa: displacement per atom):

dpa=ϕ(E)σd(E)dEt\mathrm{dpa} = \int \phi(E) \sigma_d(E) dE \cdot t

Here, ϕ(E)\phi(E) is neutron flux, σd(E)\sigma_d(E) is displacement cross-section, and tt is irradiation time.

DeviceTarget dpaNotes
ITER~3 dpaExperimental device
DEMO50-100 dpaOver lifetime
Commercial150+ dpaHigh availability operation

Helium production:

(He/dpa)1015appm/dpa(\mathrm{He/dpa}) \approx 10-15 \, \mathrm{appm/dpa}

Fusion neutrons (14.1 MeV) have higher energy than fission neutrons, resulting in higher helium production rates through (n,α) reactions. Helium accumulates in materials and causes embrittlement.

Reduced Activation Ferritic-Martensitic Steel (RAFM):

  • Representative examples: F82H (Japan), EUROFER97 (EU)
  • Composition: 8-9% Cr, 1-2% W
  • Operating temperature: 300-550°C
  • Challenges: High-temperature strength, irradiation embrittlement

ODS Steel (Oxide Dispersion Strengthened):

  • Dispersed oxide particles (Y₂O₃, etc.) improve high-temperature strength
  • Operating temperature: Extended to ~650°C
  • Challenges: Manufacturing cost, joining technology

SiC/SiC Composites:

  • Operating temperature: ~1000°C
  • Excellent reduced activation characteristics
  • Challenges: Manufacturing technology, joining, gas-tightness

Tungsten Alloys:

  • Plasma-facing material for divertors
  • High melting point (3422°C), high thermal conductivity
  • Challenges: Brittleness, recrystallization, activation

Qualification of DEMO materials requires irradiation testing with fusion neutrons:

IFMIF-DONES (International Fusion Materials Irradiation Facility - DEMO Oriented Neutron Source):

  • Generates 14 MeV-class neutrons by irradiating liquid lithium with 40 MeV deuterons
  • Accelerated irradiation of 20-50 dpa per year possible
  • Location: Granada, Spain
  • Operation start: 2030s

Significance of Power Generation Demonstration

Section titled “Significance of Power Generation Demonstration”

Power generation demonstration by DEMO is a decisive milestone in demonstrating the credibility of fusion energy to society.

In experiments up to ITER, energy extraction from fusion reactions will be demonstrated, but it will not be converted to electricity or delivered to the power grid. DEMO will be the first to demonstrate that “electricity can be generated from fusion.”

This demonstration is expected to:

  • Provide justification for continuing fusion development to policymakers
  • Prove commercialization potential to investors
  • Promote social acceptance of fusion energy

DEMO is the first fusion power plant integrating numerous subsystems:

Pnet=f(Plasma,Blanket,Divertor,Magnets,Remote Maintenance,Tritium,Power Generation)P_\mathrm{net} = f(\text{Plasma}, \text{Blanket}, \text{Divertor}, \text{Magnets}, \text{Remote Maintenance}, \text{Tritium}, \text{Power Generation})

These subsystems are individually verified in ITER and other test facilities, but verification as an integrated system will first occur in DEMO.

Key integration challenges:

  • Interface consistency between subsystems
  • Overall optimization of safety systems
  • Establishment of operating scenarios
  • Integration of instrumentation and control systems

Operating experience from DEMO provides essential data for economic evaluation of commercial reactors:

Levelized Cost of Electricity (LCOE):

LCOE=CAPEX+tOPEXt/(1+r)ttEt/(1+r)t\mathrm{LCOE} = \frac{\mathrm{CAPEX} + \sum_{t} \mathrm{OPEX}_t / (1+r)^t}{\sum_{t} E_t / (1+r)^t}

Here, CAPEX is capital cost, OPEX is operating cost, EtE_t is annual electricity production, and rr is discount rate.

Actual data from DEMO will reduce the following uncertainties:

  • Actual construction costs
  • Actual availability
  • Actual maintenance costs
  • Actual tritium fuel costs
  • Improved accuracy of decommissioning cost estimates
MilestoneEU-DEMOJA-DEMOCFETRK-DEMO
Conceptual Design Complete202720252017Under study
Engineering Design Complete203720322020Under study
Construction Start2040sAfter 2035Late 2020s2040s
Operation Start205120452035-40After 2050
Power Generation Demonstration2050sAfter 20452040s2050s

China’s CFETR shows the earliest schedule. This is due to the policy of advancing development independently without waiting for ITER results.

DEMO development is based on ITER results, but the relationship between the two is complex:

Technology transfer from ITER:

  • Burning plasma physics demonstration data
  • Superconducting magnet technology
  • Divertor technology
  • Remote handling technology
  • Test Blanket Module results

Development that should proceed independently of ITER:

  • Full-scale blanket technology
  • Steady-state operation scenarios
  • High availability achievement technology
  • Material qualification

Each region is taking the stance of “proceeding with development without waiting for ITER, while assuming ITER’s success as a prerequisite.”

Major risks for DEMO realization:

Technical risks:

  • Achieving TBR > 1 in blanket
  • Maintaining high-beta steady-state plasma
  • Long-term material durability
  • Remote maintenance system reliability

Schedule risks:

  • Design data shortage due to ITER delays
  • Material qualification delays (dependent on IFMIF-DONES progress)
  • Budget uncertainty
  • Prolonged licensing process

Cost risks:

  • Cost escalation as first-of-a-kind
  • Procurement risks for superconducting materials
  • Currency and price fluctuations

Since 2023, fusion strategies have been formulated in succession in various countries, with acceleration of development through public-private partnerships.

Major developments:

  • Japan: Fusion Energy Innovation Strategy (April 2023)
  • USA: Bold Decadal Vision for Commercial Fusion Energy (2022)
  • UK: Towards Fusion Energy Strategy (2021)
  • South Korea: Accelerated Fusion Energy Realization Strategy (2024)
  • EU: EUROfusion Roadmap Update (2023)

These strategies share common pillars of collaboration with private companies, regulatory framework development, and human resource development.

DEMO’s success opens the path to commercial reactor realization, but it cannot be commercialized as-is.

Differences between DEMO and commercial reactors:

ItemDEMOCommercial
ObjectiveTechnology demonstrationEconomic power generation
Availability30-50%75%+
Lifetime20-30 years40-60 years
EconomicsSecondaryTop priority
ScaleMediumOptimal scale
Number built1 per regionMany

Economic viability conditions for commercial fusion reactors are estimated as:

LCOE target:

LCOEtarget50100USD/MWh\mathrm{LCOE_{target}} \lesssim 50-100 \, \mathrm{USD/MWh}

This is a level competitive with current nuclear power and renewable energy (+ storage).

Capital cost guideline:

OvernightCost50008000USD/kWe\mathrm{Overnight \, Cost} \lesssim 5000-8000 \, \mathrm{USD/kW_e}

Achieving this requires significant cost reduction from DEMO:

  • Design standardization
  • Manufacturing technology maturation
  • Supply chain establishment
  • Economies of scale

Several paths are conceivable for technology development from DEMO to commercial reactors:

Evolutionary development path:

  • Gradual improvement of DEMO design
  • Economics improvement through scale-up
  • Reliable but time-consuming

Revolutionary development path:

  • High magnetic field through high-temperature superconductors
  • Transition to compact tokamak
  • Adoption of new materials (SiC/SiC, etc.)
  • Transition to advanced fuels (D-D, D-³He)

Hybrid path:

  • Parallel development of multiple technology options
  • Selection and integration according to maturity

In the 2020s, private fusion ventures have rapidly emerged. These companies are pursuing commercialization through approaches different from public programs:

Commonwealth Fusion Systems (USA):

  • MIT spin-off
  • Compact tokamak with high-temperature superconducting magnets
  • SPARC (Q > 2 demonstration) → ARC (commercial reactor)
  • Over $2 billion in funding raised

TAE Technologies (USA):

  • FRC (Field-Reversed Configuration) approach
  • p-¹¹B fuel in view
  • Over $1.2 billion in funding raised

Tokamak Energy (UK):

  • Spherical tokamak
  • High-temperature superconducting magnets
  • Achieved 100 million degrees in ST40

These ventures are pursuing commercialization through paths different from DEMO, forming multiple routes to fusion energy realization.

If multiple DEMO-class devices are operating in the 2050s-2060s and power generation demonstration succeeds, fusion power generation may occupy a share of practical power sources in the latter half of the 21st century.

Anticipated scenarios:

  • 2050s: Multiple DEMOs operating, power generation demonstration
  • 2060s: First commercial reactor begins operation
  • 2070s-2080s: Full-scale deployment of fusion power
  • End of 21st century: Fusion provides 10-20% of global electricity

Advantages of fusion power:

  • Fuel (deuterium, lithium) is virtually inexhaustible
  • Does not emit CO₂
  • Does not produce high-level radioactive waste
  • Excellent safety (no runaway reactions)

Due to these advantages, fusion is expected to contribute to both climate change mitigation and sustainable energy supply.

DEMO design is optimized based on plasma physics scaling laws.

IPB98(y,2) scaling for energy confinement time:

τE=0.0562HIp0.93BT0.15n190.41P0.69R1.97κ0.78ϵ0.58M0.19\tau_E = 0.0562 \, H \, I_p^{0.93} \, B_T^{0.15} \, n_{19}^{0.41} \, P^{-0.69} \, R^{1.97} \, \kappa^{0.78} \, \epsilon^{0.58} \, M^{0.19}

Where:

  • HH: Confinement enhancement factor (in H-mode, H1H \approx 1)
  • IpI_p: Plasma current [MA]
  • BTB_T: Toroidal field [T]
  • n19n_{19}: Electron density [101910^{19} m⁻³]
  • PP: Heating power [MW]
  • RR: Major radius [m]
  • κ\kappa: Elongation
  • ϵ=a/R\epsilon = a/R: Inverse aspect ratio
  • MM: Ion mass number

Fusion power scales as:

Pfusβ2BT4VP_\mathrm{fus} \propto \beta^2 B_T^4 V

Here, VR3V \propto R^3 is the plasma volume.

DEMO design points are optimized under the following constraints:

MHD stability:

βNβN,max2.53.0\beta_N \leq \beta_{N,\mathrm{max}} \approx 2.5-3.0

Density limit:

nenG=Ipπa2n_e \leq n_G = \frac{I_p}{\pi a^2}

Heating and current drive power:

PCD=(1fBS)IpηCDneRP_\mathrm{CD} = \frac{(1-f_\mathrm{BS}) I_p}{\eta_\mathrm{CD} \cdot n_e \cdot R}

Divertor heat load:

qdivqdiv,max1015MW/m2q_\mathrm{div} \leq q_\mathrm{div,max} \approx 10-15 \, \mathrm{MW/m^2}

Design points are searched to maximize net electric output PnetP_\mathrm{net} while satisfying these constraints.

DEMO design uses system codes that integrate physics and engineering constraints:

Representative system codes:

  • PROCESS (EU)
  • DEMO-NET (Japan)
  • SYCOMORE (EU)

These codes explore the design parameter space and identify feasible and optimal design points.

Objective functions such as power generation cost minimization or device size minimization are set for optimization:

minxLCOE(x)subject togi(x)0\min_{\mathbf{x}} \, \mathrm{LCOE}(\mathbf{x}) \quad \text{subject to} \quad g_i(\mathbf{x}) \leq 0

Here, x\mathbf{x} is the design variable vector and gig_i are constraint conditions.

DEMO (Demonstration Power Plant) is the most important milestone toward the practical application of fusion energy. Following scientific demonstration of burning plasma in ITER, DEMO will actually generate and transmit electricity, demonstrating to the world that fusion power generation is technically and economically viable.

Multiple DEMO plans are being advanced in parallel, centered on the EU, Japan, China, and South Korea. Each plan has different approaches and timelines, but with multiple DEMOs expected to operate in the 2040s-2050s, the path to commercialization of fusion power is expected to become clear.

Realizing DEMO requires solving technical challenges that cannot be sufficiently verified in ITER, including tritium self-sufficiency, high burn fraction, steady-state operation, remote maintenance, and material durability. The global fusion research community is collaborating to address these challenges.

Since 2023, fusion strategies have been formulated in various countries, and private company participation has followed in succession. With both public programs and private ventures working in tandem, expectations for early realization of fusion energy are rising.