Magnetized Target Fusion: Prospects for low-cost fusion energy
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1 Magnetized Target Fusion: Prospects for low-cost fusion energy Richard E. Siemon a, Peter J. Turchi a, Daniel C. Barnes a, James H. Degnan b, Paul Parks c, Dmitri D. Ryutov d, Francis Y. Thio e a) Los Alamos National Laboratory, Los Alamos, New Mexico 87545, USA b) Air Force Research Laboratory, Kirtland AFB, NM , USA c) General Atomics, San Diego, CA, , USA d) Lawrence Livermore National Laboratory, Livermore, CA 94550, USA e) NASA Marshall Space Flight Center, Huntsville, AL 35812, USA ITC-12 Dec 12, 2001 Toki, Japan
2 Fusion physics: o C 1 bar MTF 10 6 bar bar Partial ionization
3 Maximum pressure depends upon technology Superconducting magnets (steady state) B < 15 Tesla p < βb 2 ~ 100 atmospheres Liner technology (pulsed) B ~ 200 Tesla p ~ βb 2 ~ 10 6 atmospheres Laser compression (pulsed) p ~ atmospheres
4 Liner technology B θ ~ 100 tesla (40,000 atmospheres) 10 7 amps < 10 µs Liner is thin-walled aluminum cylinder
5 Radiograph of liner implosion Initial 1-mm thick Aluminum liner Flash xrays Side-on view of liner moving 4 mm/µs Stationary 6-mm probe jacket Elastic-plastic deformed 7-mm thick liner at 12:1 radial compression
6 How might MTF be done? 0.5 m Thin metal wall implodes Pulsed current ~ 10 7 A
7 MTF requires energy to preheat the target and separately to implode the liner Liner implosion ~ MJ Target formation and preheating ~ MJ
8 Los Alamos FRX-L experiment 3 meters 100-kV, 200-kJ Capacitor bank Current collector plate Theta-pinch coil 36-cm long; 12-cm diameter Predict n ~ cm -3 T ~ 300 ev
9 Shiva Star liner implosion (Q eff ~.01) 80 kv, 5 MJ
10 The Field Reversed Configuration
11 End-on FRC interferogram R. Siemon et al., Fusion Tech. 9, 13 (1986) M. Tuszewski, Nuc. Fusion 28, 2033 (1988) with 416 references.
12 Time history of interferograms
13 Equilibrium theory up to E ~ 5 Conducting boundary r s <β> = 1 x s2 /2 L / 2 x s = r s / R wall E = L / 2r s
14 Stability appears to depend upon elongation FRC Operating Regime Size Parameter, S* Elongation E LSX CTOR ARTEMIS FRX-L FRX-C TRX PIACE S* = 3.5 E S* = 5.8 E S* = r s / (c/ω pi ) ~ r s / ρ i E = L s / 2 r s
15 Profile of long FRC determined by equilibrium alone D.C. Barnes, Phys. Plasmas 8, 4864 (2001) Combining p = p(ψ) with uniform elongation ( / z << / r) gives solution p = [ ψ ; ( ˆ) ] 2 p0[ ψ ; pop] + ε p1 r s z Depends on: open p ; elongation ; shape p 0 -p s curves essentially the same r ψ Universal closed pressure z 25:1 2D solution
16 S* [ E Stability with Hall terms agrees with empirical good parameter regime* H P H E [ B H B BB P B H BB B P P PPP P PP PBB P C E F [ E F [ [ B P F H E FRX TRX PIACE LSX CTOR C ARTEMIS E FRX-L S*/E Empirical analysis (Tuszewski) shows S*/E < 3.5 for good plasma flux confinement. Theory shows S*/E < 2-4 for stability [ Eql. 1 Eql. 2 Eql. 3 Eql. 4 Local Volume average S* = r s /(c/ω pi ) E = l s /d s *D. C. Barnes, Phys. Plasmas, accepted Nov. 2001
17 Los Alamos FRX-L team Goal: Compress an FRC inside a liner to achieve T ~ 10 kev
18 Los Alamos Atlas facility (Q eff ~ 1) 240 KV 25 MJ
19 Summary of introductory points The field-reversed configuration provides one method to position 300-eV plasma inside a conducting cylinder Recent theoretical work suggests that the long-standing paradox of FRC stability might now be resolved Liner implosions with 10:1 radial compression are feasible B ~ 50 kg ~ 5 x 10 6 G P ~ 100 bar ~ 10 6 bar (1 bar = 1 atmosphere) One should ask: Why is this important to fusion research?
20 High pressure cavity 10 kev plasma mixed with magnetic field xr R dr Pusher material with density ρ α = dr/r B nt r
21 Lawson triple product requirement ½ n 2 <σv> E f 3nT/τ E ; ρ = n m i ntτ E 6T 2 / <σv> E f Temperature and fusion cross section σ determine required product of pressure and energy confinement time
22 System size tends to decrease as pressure increases Suppose τ E is determined by thermal diffusivity; then size must be large enough to meet Lawson condition: τ E = a 2 /χ Define an engineering β =nt/ P a = sqrt(τ E χ) = sqrt(ntτ E χ/β) / sqrt(p)
23 Variation of size with pressure depends upon specific loss processes Fuel Mass (grams) ITER Advanced concepts Approximate Upper-limit Bohm MTF Diffusion-limit classical magnetic confinement Diffusion-limit Zero magnetic field NIF Fuel Energy (joules) Pressure (atm.)
24 Dwell time Pressure (P) lasts for a pulse time τ limited by inertia of liner (density ρ). τ =dr/ (P/ρ) 1/2 Pulse duration τ must separately satisfy the Lawson condition.
25 Liner kinetic energy and power Can show: E = E plasma + E field = (1+βx 2 /2) PV Kinetic Energy is related to E by an efficiency ε KE = E/ ε Characteristic Power = E / τ
26 Cost estimate State-of-the-art pulsed power devices: NIF $6 / megawatt Z machine $3 / megawatt Atlas $12 / megawatt Adopt $1/joule and $10 / megawatt for this type of pulsed-power supply Make estimate: MTF cost ($) = $1 * KE(J) + $10 * Pwr(MW)
27 Generic MTF facility cost vs. pressure Cost ($Millions) ITER-FEAT FIRE NIF Z Atlas Generic MTF Generic Tokamak High pressure tokamak 10 1.E+02 1.E+04 1.E+06 1.E+08 1.E+10 1.E+12 Pressure (atmospheres)
28 Energy confinement specific targets ICF: electron thermal conduction χ = λ v e λ = m.f.p., v e = elec. thermal speed Field Reversed Configuration: empirical scaling χ = ρ i v o ρ i = ion gyro radius v o = 4x10 6 cm/s Wall-confined Bohm thermal conduction χ = ρ i v i / 16
29 Facility costs - specific plasma targets Cost ($Millions) NIF Z Atlas Generic MTF ICF FRC Q ~ 1 Bohm Q ~ E+04 1.E+06 1.E+08 1.E+10 1.E+12 Pressure (atmospheres)
30 Wall-confined Bohm-like plasma Pusher material with density ρ α = dr/r R dr L R 10 kev plasma mixed with magnetic field
31 Computations show wall-confined plasma cools at acceptable rate 5x10 19 cm -3 1 kev Z n T θ Z θ r 3 cm 3 cm 50 T B θ pinch B z Z pinch B θ 2x10 4 bar P Z θ 3 cm 3 cm
32 Russian MAGO has wall-confined plasma Inverse pinch acceleration Nozzle action
33 Ground Conceptual experiment to study wall-confined plasma T ~ 0.5 kev n ~ cm -3 I 1 MA ~ 0.1 µs Insulator Inverse pinch current sheet Aluminum 5 cm Center-line
34 Program plans DOE Office of Fusion Energy Sciences Exploratory Research Develop FRC target plasma FY $2-4 M / year Proposed: Liner implosion Shiva Star FY $4-6 M / year Liner implosion Atlas FY $10-20 M / year NASA Marshall Space Flight Center Plasma-gun implosion system FY $2-3 M / year Actual budgets in black Anticipated budgets being proposed in red
35 Technical issues Plasma target formation, stability, and energy confinement at high density Wall-plasma interactions and impurity mixing with fusion fuel Gain limitations using batch-burn mode Practicality of pulsed operation
36 Conclusions MTF warrants exploration given its potential as a low-cost approach to fusion The cost results are derived from simple considerations and experience with pulsed-power facilities; not plasma physics. Plasma physics will determine the detailed behavior and ultimate optimization of an MTF system. Experimental facilities already exist that allow testing of many critical MTF issues This research is just beginning; interested scientists are encouraged to contact any of the authors (more information at
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