multi-recycling of plutonium and ma in pwr using hydride...
TRANSCRIPT
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Multi-recycling of plutonium and MA in PWR using hydride fuels
Thursday 16th March 2009
Francesco Ganda – Ehud Greenspan
The 5th Joint Reactor SeminarGoNERI, The University of Tokyo
andNuclear Engineering Department, UC Berkeley
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Is it possible to multi-recycle Pu in PWR?
MOX allows multi-recyclings only up to about 12w/o Pu: after that the large void reactivity coefficient becomes positive.This happens after 2-3 recycles.
Solutions proposed up to now:
CORAIL, MOX-UE, CONFU (all TRU).
All use 235U to reduce plutonium mass, either homogeneously or heterogeneously mixed.
Drawbacks-) reach Pu (or TRU) stabilization, not net destruction; -) large power peak for heterogeneous configurations;-) no substantial U or SWU saving over conventional UO2.
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Our solution:
Use hydride fuels, of the type:
Ux-ZrnH1.6n-ThmH2m-PupH2p (-MAqH2q)
The rationale:
The extra H in the fuel (Hfuel~Hwater) will increase plutonium (and MA) destruction through a softer spectrum and will
counteract the effects of large voiding.
10-2 10-1 1000
0.005
0.01
0.015
0.02
0.025
0.03
0.035
0.04
0.045
0.05
Neutron Energy (eV)
Neu
tron
flux
UO2P UZHMOX
Beginning of Life
10-2
10-1
100
0
0.005
0.01
0.015
0.02
0.025
0.03
0.035
0.04
0.045
0.05
Neutron Energy (eV)
Neu
tron
flux
UO2P UZHMOX
End of Life
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Design variables
-) Fuel cycle scheme (total or partial recycling of U, Pu, Np etc…)-) Fuel composition: mixture of ZrH1.6, ThH2, U in various amounts-) Possible use of burnable poisons-) Possible use of different U enrichment
Assumptions
-) Instantaneous reprocessing-) 0.1% of U and Pu is lost during reprocessing-) 0% losses during fabrication and irradiation-) Feed Pu vector is fixed (from 1)-) Feed MA vector is fixed (from 2)
1 Youinou, G. and Vasile, A., 2005. Plutonium Multirecycling in Standard PWRs Loaded with Evolutionary Fuels. Nuclear Science and Engineering: 151, 25-45. 2 ANL ICONE 10-22575, Table 1 col. b, based on “extended PWR benchmark with 10y cooling”
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Constraints
-) Negative core-average burnup-dependent reactivity coefficients (fuel temperature, coolant temperature, small void, large void)
-) Similar cycle time (1430 EFPD) and control system of standard UO2-) Same fuel D and P/D of standard UO2
Unit Cell Geometry and Specific Power
Hydride Fuels Oxide Fuels
Clad outside diameter 0.95 cm 0.95 cmP/D 1.3261 1.3261
Fuel diameter 0.8192 cm 0.8205 cmClad inside diameter 0.8357 cm 0.8357 cm
Pitch 1.26 cm 1.26 cmSpecific power 76.715 W/giHM 36.138 W/giHM
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Methodology
TRITON/NEWT code is used for depletion analysis, extensively tested for degraded plutonium and MA–bearing fuels, both in
numerical benchmark and in measured samples (long experience with SAS2H).
BONAMI/NITAWL: XSEC pre-processingNEWT: transport, 3-groups XSEC collapsing
ORIGEN-S: 0-D depletion and decay
Transport calculations performed with 238 energy group, directlyincluding 40 actinides, 187 fission products.
More nuclei are followed using ORIGEN-S default XS.
Pu amount is adjusted exactly to match desired cycle length Two steps approach for greater precision:
1. Two runs that over and under estimate cycle length;2. Final run to estimate discharged and cooled composition.
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Methodology – types of fuels analyzed for Pu recycling
PuH2-ZrH1.6-U (uranium varies from 0 g/cm3 to 3.72 g/cm3)PuO2-ZrO2-UO2 (uranium varies from 0 g/cm3 to 8.28 g/cm3)
In both fuel types the U amount is fixed*, the plutonium is adjusted to reach the desired cycle length, the remaining space is taken by zirconium in the appropriate chemical form (hydride or oxide). If the zirconium is zero and more space is needed, uranium is taken out in the desired amount.
For Th-based fuels, ThH2 replaces U. Same methodology.
* The depleted uranium amount is initially fixed at a pre-assigned value, after depletion the entire uranium amount is recycled, adding new depleted uranium if:-) needed to make up for the consumption-) needed to reduce enrichment below 20% 235U or 12% 233U
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Methodologyhydride fuels for Pu + Np or TRU recycling
PuH2-NpH2-(MAH2)-ZrH1.6-U (uranium varies from 0 g/cm3 to 3.72 g/cm3)
Same methodology as before to fill the fuel volume.PuH2 has a density of 10.4 g/cm3, not much is known of hydrides of MA, so it is assumed that the density will be the same* as for PuH2. The density is not adjusted to account for varying isotopic composition*.
When a given amount of Pu is taken from LWR spent fuel, a proportional amount of Np (or MA) is taken as well, according to the following vector**:
U, Np, Pu, Am, CmMA_frac=[0.003810517, 0.07691684, 1, 0.07117211, 0.006312254];
*recommended by prof. Olander**from ANL ICONE 10-22575, Table 1 col. b, based on “extended PWR benchmark with 10y cooling”
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Fuel cycle scheme with plutonium recycle
Fuel fabrication
Reprocessing (Pu, U separation)
Final repository
Reactor (irradiation)
Depleted U Spent LWR fuel
Pu
Reprocessing (Pu separation)
99.9% of Pu, U
100% of FP 0.1% of Pu and U100% of MA
10 y cooling
100% of FP 0.1% of Pu100 % of U100% of MA
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Fuel cycle scheme with plutonium and neptunium recycle
Fuel fabrication
Reprocessing (Pu, U, Np separation)
Final repository
Reactor (irradiation)
Depleted U Spent LWR fuel
Pu, Np
Reprocessing (Pu, Np separation)
99.9% of Pu, U, Np
100% of FP 0.1% of U, Pu, Np100% of other MA
10 y cooling
100% of FP 0.1% of Pu, Np100 % of U100% of other MA
Results: selected characteristics of PUZH and MOX with variable uranium loadings at First Recycle
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U % of total in PUZH* 0% 25% 50% 75% 100% Standard MOX
PUZH TRU destruction fraction 64.36% 54.13% 47.83% 42.39% 37.48%
32.56%
46.13%
49.65%
MOX TRU destruction fraction 63.65% 49.76% 42.65% 37.11%
--23.7%
--PUZH Fissile fraction at EOL 21.63% 32.87% 38.52% 42.74%
MOX Fissile fraction at EOL 24.50% 38.05% 43.39% 46.99% 60.3%* maximum uranium in PUZH: 3.7203 g/cm3
Fraction of maximum uranium in PUZH* Standard MOX
0% 25% 50% 75% 100% --
Rho U (g/cm3) 0 0.9301 1.8601 2.7902 3.7203 8.4612
Rho Pu (g/cm3) 0.7337 0.7564 0.7791 0.8018 0.8245 0.8038
Rho HM (g/cm3) 0.7338 1.6865 2.6392 3.592 4.5448 9.265
Rho fuel (g/cm3) 5.9415 6.6087 7.2759 7.9432 8.6104 10.465
H/HM 82.04 34.89 21.85 15.73 12.18 3.9
Burnup (GWD/MTiHM) 628.4 284.2 182.1 132.6 102.9 54.66
EFPD 1376.0 1430.1 1434.3 1420.9 1395.8 1512.45
Characteristic
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Results: TRU destruction fraction
20.00%
30.00%
40.00%
50.00%
60.00%
70.00%
80.00%
0% 20% 40% 60% 80% 100%
Volume percent of the maximum loadable
TRU
dest
ruct
ion
fract
ion PUZH
TPZHMOX
0.00%
10.00%
20.00%
30.00%
40.00%
50.00%
60.00%
70.00%
0 20 40 60 80 100H/HM
TRU
des
truc
tion
frac
tion
PUZHTPZHMOX
• TPZH = ThH2-PuH2-ZrH1.6; • PUZH = PuH2-U-ZrH1.6; • Maximum loading is Th for TPZH and U for PUZH and MOX,• 100% is for PUZH, not MOX (which can load higher U amounts)
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Results: Fuel temperature coefficient of reactivity (FTC)
-3
-2
-1
0
1
2
3
4
0 100 200 300 400 500EPFD
FTC
(pcm
/K)
FTC with HSeries3
-3
-2
-1
0
1
2
3
4
0 500 1000 1500EPFD
FTC
(pcm
/K) FTC with H
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Results: Fuel temperature coefficient of reactivity (FTC)
-3
-2
-1
0
1
2
3
4
0 500 1000 1500
EPFD
FTC
(pcm
/K)
FTC with HFTC with D
-3
-2
-1
0
1
2
3
4
0 100 200 300 400 500EPFD
FTC
(pcm
/K)
FTC with HFTC with DS i 3
10-5
100
105
1010
0
0.02
0.04
0.06
0.08
0.1
0.12
0.14
0.16
0.18
Neutron Energy (eV)
Neutron flux per unit lethargy
ZrD1.6-P uD2ZrH1.6-P uH2
FTC of PUZH Burnup-dependent FTC<0 for U>25%.
ButFTC>0 for U=0 during the 3rd batch.
Solutions-) burn only up to 2nd batch-) Use D instead of H
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Selected results: TRU destruction fraction as a function of recycle number
PUZH (left) MOX (right)
0 5 10 15 20 25 30 350.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
Cycle Number
TRU destruction fraction
U 0%U 25%U 50%U 75%U 100%
0 2 4 6 8 10 12 140.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
Cycle Number
TRU destruction fraction
U 0%U 11.2%U 22.4%U 33.7%U 44.9%U 64.2%U 83.6%U 100.0%
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Results: PUZH, 33rd recycle: core-average FTC, and LVRC (90%)
without soluble boron
0 50 100 150 200 250 300 350 400 450 500-3.4
-3.2
-3
-2.8
-2.6
-2.4
-2.2
-2
-1.8
EFP D
FTC (pcm/K)
U 0%U 25%U 50%U 75%U 100%
0 50 100 150 200 250 300 350 400 450 500-30
-20
-10
0
10
20
30
40
50
60
EFP D
LVRC (pcm/% void)
U 0%U 25%U 50%U 75%U 100%
Major finding:The LVRC of PuH2-ZrH1.6 remains negative throughout the recyclings!
NOTE: with 100% void LVRC becomes positive, but core leakage compensates
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Results: MOX, 13rd recycle: LVRC (90%)
with soluble boron (left) and core-average without (right)
0 500 1000 1500120
140
160
180
200
220
240
260
EFP D
LVRC (pcm/% void)
U 0%U 11.2%U 22.4%U 33.7%U 44.9%U 64.2%U 83.6%U 100.0%
0 50 100 150 200 250 300 350 400 450 500130
140
150
160
170
180
190
EFP D
LVRC (pcm/% void)
U 0%U 11.2%U 22.4%U 33.7%U 44.9%U 64.2%U 83.6%U 100.0%
whileThe LVRC of PuO2-ZrO2-(U) becomes positive at the 13th recycling
Conclusion:Possible To Indefinite Recycle Pu In PWR Using Hydride But Not Oxides
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Results: PuH2-NpH2-U-ZrH1.6 TRU destruction fraction (left) and
fissile fraction at discharge (right) as a function of recycle number
0 2 4 6 8 10 12 140.1
0.15
0.2
0.25
0.3
0.35
0.4
0.45
0.5
0.55
0.6
Cycle Number
TRU
des
truct
ion
fract
ion
U 0%U 25%U 50%U 75%U 100%
0 2 4 6 8 10 12 140.25
0.3
0.35
0.4
0.45
0.5
Cycle Number
Pu
fissi
le fr
actio
n
U 0%U 25%U 50%U 75%U 100%
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Conclusions
-) It is found possible to infinitely recycle Pu in PWR using as feed only depleted uranium and Pu coming from LWR spent fuel, provided that most of the excess reactivity will be compensated by means other than soluble boron.
-) MOX, on the other hand, only allows recycling up to 9-10 times.
-) The TRU destruction fraction, >60% for first recycle, stabilizes at ~20% at equilibrium.
-) It appears possible to multi-recycle up to 8-12 times Pu and Np in PUZH fuel (corresponding to 110-170 years).
-) All-TRU recycle in U-based hydrides appears feasible only up to few recycles (2-3).
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Thank you
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Results: TRU-H2-U-ZrH1.6 TRU destruction fraction (left) and fissile fraction at discharge (right) as a function of
recycle number
0 5 10 15 20 25 30 35 40 450
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
0.45
0.5
Cycle Number
TRU
des
truct
ion
fract
ion
U 0%U 25%U 50%U 75%U 100%
0 5 10 15 20 25 30 35 40 450.25
0.3
0.35
0.4
0.45
0.5
0.55
0.6
Cycle Number
Pu
fissi
le fr
actio
n
U 0%U 25%U 50%U 75%U 100%