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FFR_chap22.txt
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CHAPTER 22
CHEMICAL PROCESSING*
22-1. INTRODUCTION
The Liquid Metal Fuel Reactor offers the opportunity for continuous
removal of fission products from the fluid fuel by chemical and physical
processing. By this procedure the poisoning effect of the fission products
may be kept to a low level, and thus make possible a good breeding ratio
in this thermal reactor. In this chapter, the various chemical and physical
processes for removing the fission products are discussed.
To simplify the discussion, the fission products are classified into four
basic groups ax follows:
(1" Gaseous elements or compounds that are volatile at reactor operat-
mmg temperature. This group is ordinarily abbreviated FPV.
(21 Nonvolatile elements forming compounds more stable than the cor-
responding uranium compound. The abbreviation for this group is FPS.
(3 Nonvolatile elements forming compounds that are less stable than
the corresponding uranium compound and more stable than the correspond-
ing bixmuth compound. The abbreviation for this group is FPN.
i+ Nonvolatile elements forming compounds less stable than the cor-
rexponding bismuth compounds. The abbreviation for this group is NFPN.
In the PV group there are four elements: bromine, iodine, krypton,
and xenon. Of these, 6.7-hr I35 and its daughter 9.13-hr Xe!3® are the
imporrant ones. Xe!33 is by far the most important because of its cross
section, 2,700,000 barns. Since this is so large, it is necessary to remove
mo~t of the 1odine and xenon as soon as formed.
The other major poisons occur in the I'PS group. In calculating the
average atomic weight and cross section of these groups, it is convenient
to us¢ the fission yield in milliatoms. Normally, it is assumed that two
atoni~ of fission products are produced by the splitting of one atom of
uranium. Thus, 2000 milliatoms of fission products are produced by fission
of one utom of uranium, and 1% yield is equal to 10 milliatoms. On this
basix, Tuble 22-1 presents the FPS nuclides with the important informa-
tion on their poisoning effect. As can be seen, Sm!*¥ is the most important
element to be dealt with in this group.
The last group, commonly called the noble fission products, represents
a combination of groups (3) and (4} in the above classification. The im-
portant polsoning information on all these nuclides is given in Table 22-2
*Based on contributions by O. E. Dwyer, A. M. Eshaya, F. B. Hill, R. H. Wiswall,
W. 5. Ginell, and J. J. Egan of the Brookhaven National Laboratory.
791
TasLeE 22-1
Fusep-SaLT SoLusLE Fisston Pronuers [1]
Precursors have half-lives less than 5 days.
\ I
Fission | Cross sec- l
Nuclide Hali-life vield y, |tion g, barns yo T.ype
milliatoms® (at0.025ev) § poison]
Rb#3 Stable 20 (.90 18 3
Rh#0 19d 36 1.0 36 3
RE®7 6.2 X 1010y 46 0.14 6.4 3
Sré8 Stable o4 0.005 0.25 3
Sré¢ H4d 61 110 6,700 2
Sro0 20v 64 1.0 64 .0 3
Y —7r%! 6i1d; (stable) 66 1.52 100.0 3
Xe—(g!33 5.27d 66 29 .0 1,920 3
(stable)
(4135 3 X 106y i 70.5 15.0 1,060 3
(Csld7 37y 71.5 2.0 143 3
Bal3® Stable 71.1 0.6 43 3
Lal3® Stable 70.5 8.4 290 3
Ba—La—(Cel40 12,8 40h 68 .5 0.63 43 3
{(stuble)
(Ce —»Pri4! 32d (stable)! 61.5 11.2 68K 3
(Cel42 Stable 55.0 1.8 99 3
Pr—Ndi43 13 5d 45.5 290.0 13,200 2
(stable)
Ce—Pr—-Ndlit 280d; 17m 36.0 4.8 173 3
(stable)
Nj14s Stable | 27 0 52.0 1,400 2
N (146 Stable 200 9.8 196 3
Nd —Pm—Sm!? 11.6d:2 Gy 14.0 60.0 840 2
(stahle)
Ndi8 Stable 1.0 3.3 33 3
Smle Stable 7.0 | 47,000 329,000 1
Ndtso Stable 5.0 2.9 14.5 3
Smial 73y 2.6 7,200 18,700 1
Smis2 Stable 1.6 150 240 2
Euls3 Stable 0.9 420 378 2
Smiot Stable 0.5 5.5 2.8 3
Eytse 17y 0.3 | 13,000 3,900 1
ou—(Gdles 15d (stable) 0.2 730 150 2
Gdts7 Stable 0.1 |160,000 16,000 1
Total 30 nuclides 10523 394,010
*Percent vield multiplied by 10; total yvield is 20097, or 2000 milliatoms.
10 avg = 374 barns,
fo > 1000 = type 1; o 50 to 1000 = type 2; ¢ < 50 = type 3.
22-11 INTRODUCTION 793
TasLE 22-2
Fusep-Sanr InsoruBLE Fissron Probpucts [1]
Fission Cross sec-
Nuclide Half-life vield y, Ition &, barns ya T}.’pe
milliatoms |(at 0.025 ev)t potson
Se’? Stable 0.4 40 16 2
Se’8 Stable 1.1 0.4 4.4 2
Se™® 6 X 104y 2.0
Seso Stable 2.8 0.53 1.5 2
Se82 ~Stable 5.5 0.055 0.3 2
7r92 ~table 67.5 0.25 17 2
Zr93 5 X 108y 68.0 3 204 2
7irtd Stable 67.5 0.08 5.4 2
LN 65d; 37d 660 13 .4 880 2
o | Stable 64 .0 0.05 3.2 2
N i Stable 59.0 2.10 124 2
Mo j Stable 56.0 013 7.2 2
Tt 2.1 X 10%y 48.0 100 4,800 1
SN Stable 35.0 0.2 7.0 2
Rua'™ stable 2060 12 312 2
Rt Stable 24 .0 1.2 29 2
Ruis 40d 88 150 1,320 !
Ru NUIL* Stable 6.2 0.7 4 2
Pifios | Stable 4.6 18 83 2
SRR | 1.0y 3.3 (15)1 (50) (2)
P A% 10% 2.2 750 1,650 1
Pt . Stable 1.3 11.1 14 2
A ! Stable 0.9 84 75 2
- P NLTL Stable 0.4 0.4 0.2 2
S Stable 0.3 750 225 1
SR ‘ Stable 0.2 0.03 0.01 2
C i stable 0.2 25,000 5,000 1
b | Stable 0.2 3.86 0.76 | 2
SN T | Stable 0.4 0.2 0.081 2
= =h=Tel?d 10d; 2.7y (stable) 0.6 1.5 (.90 2
T | Stable 0.9 0.8 0.72 2
" Tel ‘ Stable 5.7 0.16 0.91 2
C Tet ! Stable 25.0 0.31 7.8 2
Taotal 33 i 654.0 14,843 .38
*N.I.. not identified as fission product on G.I8. Chart, 1952,
T0 e = 22.7 barns.
*Assumed from values for daughter, Pd!98.
794 CHEMICAL PROCESSING [cHAP. 22
under the group heading FPN. As can be seen by examining the column
headed yo, none of these nuclides is & very important poison, compared
with xenon and samarium.
From the data given in these tables, it is possible to calculate the poison
level in an LMFR as a funetion of time of operation. Besides the charac-
teristics of the fission products themselves, the poison level is dependent
mainly on the core fuel volume, the total fuel system volume, and the
average core flux. In Fig. 22-1, the poison level is given as a function of
days of operation for a 500-Mw LMFR reference design [1] with 600 ppm
U233 in Bi. It is assumed that the volatile poisons, FPV, can be removed
in a steady-state operation and the poisoning level kept to 19%. The other
two classes, of course, steadily increase, based on the assumption of no
chemical processing of the core. After a certain poisoning level is reached,
the continuous chemical processing will serve to keep the poisoning at a
constant value. This level must be chosen by a careful economie optimiza-
tion procedure.
Figure 22-1 shows that while the FPS group is the most important, as-
suming that the volatiles can be removed as desired, the FPN group does
gradually accumulate, and after about 400 days of operation has a 1%
poisoning effect. Hence, over long-term operation, processing of all the
groups becomes desirable if a low poison level is to be maintained.
The poisoning in a U?*-fueled reactor is expected to be 10 to 20%
higher than in a U#*3-fueled reactor [2,3] depending on the average resi-
dence time of the fission products in the fuel. This is due to a shift in the
fission product spectrum toward higher cross section nuclides. The cu-
mulative poisoning effect of the higher uranium isotopes is also slightly
higher for 17233,
In connection with this last point, the higher isotopes of uranium grad-
ually build up throughout the operation of the reactor. In the calculations
used in the reference design of Chapter 24 and in BAW-2 [1], the poison-
ing effect of the higher uranium isotopes has been assumed as 2% for a
U233 fuel. Since these higher isotopes are chemically the same as the fuel,
no provision can be made for a chemical separation from the U233, The
gradual buildup of the higher uranium isotope poisons can actually be
tolerated over a number of years before becoming important in the eco-
nomics of the reactor operation, as is shown in Chapter 24,
In all the foregoing discussions, it is assumed that corrosion products
contribute very little to the poisoning in the reactor. However, this may
not be so. As was described in Chapters 20 and 21, the corrosion rate of the
containing metals by the bismuth fuel is rather high. Corrosion products
such as iron and chromium at a concentration of 300 ppm in bismuth would
contribute a poisoning effect of about 19;,. However, the same processes
which remove the FPS and I'PN will also remove all the corrosion products.
22-2] VOLATILE FISSION PRODUCT REMOVAL 795
%
Poison,
—-"_——-
N - - FPN ’—__..__——"
- -—/-- -
- // /"/ —
--——‘-" FPV {Assumed
__—“--..fi _______ D SR ST I SRR SISl w— o ekt el WP VRVD sy D P R AR .
. | | i I | | ] |
200 400 600 800 1000 1200 1400 1600 1800 2000
Time of Operation, Days
Fic. 22-1. Poison level after startup vs. time of operation for all fission products.
Core fuel volume, 1800 ft3.
22-2. VoraTiLE FissioNn Propuct ReEmovarn [20]
22-2.1 Xenon and iodine removal. For a 19, poisoning level, assuming
1o Xe adsorbed on, or absorbed by, the graphite moderator, the concen-
trations of 9.13-hr Xe!35 and total Xe in the fuel are calculated to be 1.5 and
124 ppb. respectively. Compared with the 9.13-hr Xe!35, the combined
poi=ouing effeet of all the other FPV’s is negligible, so that the problem
of FPV removal is really one of Xe!35 removal. Some typical statistics on
the FPV s are summarized in Table 22-3. These figures are based on three
w==nmptions: (a) that Xe buildup on the graphite is negligible, (b) that
nealicible amounts of Br and I are volatilized with the FPV’s; and (¢) that
Ivr wd Xe have the same removal characteristies.
Lo Article 20-3.3 it was shown that the actual solubility of xenon in
bisrth may well be in the ppb range; McMillan caleulated the solubility
.= 10 <. Sinee the amount of xenon generated is probably larger than its
<ol in bismuth, it is necessary to determine the behavior of the gas
. relution to the surfaces of the reactor core and fuel conduits, as it will
biove oo strong tendency to escape from solution.
~ince the xenon is the decay daughter of I'35, it is born not only in the
reostor core but throughout the fuel system wherever 135 is present.
Therefore the chemical and kinetie behavior of I, its decay precursor, 1s
inportant. The Xe!'3® removal problem might be solved by desorp-
rion of 19 however, it is found that the I'3° deecays so rapidly that
ot eust 7o0 of the I'5 would have to be removed with the IFPV’s in
796 CHEMICAL PROCESSING [cHAP. 22
TaBLE 22-3
STtaTisTICS ON FPV’s unpER CONDITIONS OF
19, Rreacror PorsoNing For A 500-Mw Rreactor
1000 ppm U233, 150 tons of Bi
1. Concentrations, ppb
(a) Kr 2.8
(b) 9.13-hr Xe!3% 1.46
(¢) Total Xe 12.9
(d) Total FPV’s 15.7
2. Removal rates, g/day
(a) Kr 23.1
(h) 9.13-hr Xel!35 12.0
(¢) Total Xe 106.0
(d) Total FPV’s 129.1
3. Per cent, by weight, total fission products 23.8
4. Average atomic weight of FPV's 122.3
5. Rate of radiant cnergy release, kw/g 605
order to significantly reduce the amount of Xe'35 formed. This is probably
too much to be hoped for. Tixperimental results indicate that such a large
fraction of the 1 cannot be volatilized from U-Bi fuel. Thermodynamic
analysis indicates that the I, for the most part, should react with the Rb,
Sr, Cs, and Ba fission products to form monoiodides with about 709 of the
I going to Csl.
These alkali and alkaline-earth iodides would presumably have low solu-
bilities in Bi and, as a result, have a tendency to leave the U-Bi fuel and
collect on unwetted solid surfaces. These 1odides also transfer heavily to
the salt in the I'PS-removal process, but the rate of processing would be
too slow to extract significant quantities of 135 and, in fact, most of the
other 1odine nuclides. Thus there appear to be two predominant modes
by which I departs from the fuel: physical expulsion in the form of iodides
and radioactive decay,
22-2.2 Xenon and iodine adsorption on graphite and steel. Graphite is
not wet by the fuel; moreover, 1t has a void volume of almost 209, largely
composed of interconnected cells. These facts suggest the possibility of Xe
buildup in an LMITR core.
A factor in this problem is the behavior of iodine i the LMIR fuel.
The 1odine may form rather insoluble iodides, then adsorb on unwetted
surfaces, and there decay to Xe. Both kinetic and thermodynamic analyses
indicate that this may be a real possibility.
22-2] VOLATILE FISSION PRODUCT REMOVAL 797
In 1956, an in-pile loop [4] was operated at Brookhaven in which fission
products were gencrated in U-Bi fuel, where the natural U concentration
was 800 ppm. The concentrations of fission products were therefore
several orders of magnitude below those for an LMEFR. Two steel rods,
1,2 in. in diameter and 4 in. long, were suspended vertically in the gas
space of the surge tank, 2 in. above the liquid metal level. One was exposed
for a period of 60 hr and showed an I'¥ concentration of 9.0 X 107 atoms/
em? at time of removal; the other, exposed for 85 hr, showed 1.6 X 107
atoms/cm2. The corresponding I'#2 concentration in the flowing metal
was 1.1 X 10¢ atoms,cm?®, which means that for every 100 atoms of 1!33
per cc of fuel there were roughly 1 to 8 I'¥ atoms/cm? of exposed surface
in the gas space. The temperatures of the rods and liquid metal were the
same, H00°C.
Several steel tubs immersed for extended periods in the flowing metal
showed 1'%* concentrations on their surfaces roughly 100 times those found
on the rods =uspended in the gas phase. Moreover, it was estimated that
less than half the T in the system was in the Bi; about 60%, was found on
the container walls contacting the Bi and about 197 on the gas walls. The
tabs were. for the most part, unwetted by the Bi.
The loop had a degassing chamber in which the metal flowed in a thin
Javer over a baffled plate. Samples of gas taken from this chamber showed
I concentrations too small to measure, even radiochemically.
To get a better understanding of this general problem, a two-part ex-
perimental program is underway at BNL. In the first part, capsule scale
experiments are heing carried out to determine the action of iodine and
xenon on graphite and steel capsules containing U-Bi fuel. These capsules
are irradiated in the BNL pile and then examined for iodine, xenon, and
rudioacetivity across the radius of the specimen. The second part of the
prograin i= a kinetic study of the removal of iodine and xenon in degassing
equipnient.
[r-pile capsile experyments. In one series of experiments, capsules made of
2L (r=17, Mo steel and graphite were filled with Bl containing 500 to
1000 ppra of natural U, 350 ppm Mg, and 350 ppm Zr. The capsules were
degas=cd under vacuum for 3 hr at 800°C before being filled. They had the
dimensions 1.27 em ID, 1.60 em OD, and 10 e¢m long. The capsules were
irradiated in o flux of 2 X 10'2/(em?)(sec), with the U-Bi mixture frozen,
for periods up to 2 wk. After irradiation, the capsules were held at 500°C
for periods ranging {from 10 min to 117 hr. They were then cooled quickly
to room temperature and sectioned into 10 disks for radiochemical analysis.
The concentrations of Xe!33, 1133 and U were measured at the center of
each disk and in a 1-mm ring on the periphery of the Bi. The results are
summerized in Table 22—4.
These experiments are exploratory. They were carried out to determine
798 CHEMICAL PROCESSING [cHAP. 22
TaABLE 22-4
REsurts or IN-PILE STUDIES ON THE
BEnavior or IopiNeE aANnD XENON IN LMFR FukL
Concentration Concentration '
of 1183, of Xe!33, Agitated
Sample Contaiper atoms/g Bi atoms/g Bi during
number | material equilibration
Core | Periphery | Core | Periphery time
S-010 steel AX 108 1 5x 10" | 7x 107 | 6 x 101! No
S-020 " 7x 108 | 2x 101 | 2x 101 | 7 x 10U i
G010 graphite | 2 X 10 | 6 x 101! — — ”
G-020 ” 2x10° | 1x 10" | 2x 10° | 2 x 100 ”
G030 ” 4x 108 | 2x10° { 1x 109 | 2x 10° ”
G040 ” 3 X109 | 3 x 104 | 1 x 1080 | 4 x 100 ”?
G080 Y 5X 1010 | 3x 101 | 2x 10° | 7 x 10° Yes
G-150 ” 7X 100 6x 10" 1 x 10° | 7x 10° ”
roughly the extent to which iodine and xenon concentrate on interfaces.
However, in spite of the limitations of the experiments, the following con-
clusions are warranted.
When the concentration of iodine generated by fission reaches a level of
about 10'! to 10'? atoms/g Bi (capsules S-010, 8-020, G-010, G-020), the
lodine concentrates at the interface hetween the Bi and the container wall.
The concentration at the interface is about 1000 times higher than that in
the bulk of the Bi for the steel capsules, and about 100 times higher than
that for the graphite capsules.
When the concentration of Xe reaches a level of about 101! to 10'2
atoms/g Bi (capsules S-010, S-020, G-010, G-020), its concentration near
the Bi-steel interface is about 10,000 times that in the Bi. This ratio for
graphite, G, 1s only 10 (G-020). The difference between the steel and graph-
ite capsules is believed to be due to the fact that Xe diffuses into the latter.
This penetration by fission-product gases has been found in other experi-
ments and confirmed by autoradiographs and material balances.
When the concentrations of iodine and Xe are lower, ie., about 10°
atoms/g, the differences between interface and core concentrations are
much smaller, though still statistically significant (Xe in G-040, iodine
in G030 and G-040). For iodine the concentration ratios vary slightly
from less than 10 for G-030 to 100 for G-040. For Xe the ratio is only about
3 for G040, and no significant, separation was observed in G-030. These
22-2] VOLATILE FISSION PRODUCT REMOVAL 799
Fig. 22-2, In-pile capsule experiment with molten bismuth fuel, showing xenon
and 1odine diffusion into graphite.
lower Xe ratios are again attributed to the loss of Xe from the interface to
the graphite.
Samples G-080 and G-150 were agitated (by rotating them at 15 rpm
around an axis passing at right angles through the middle of the capsule)
while being equilibrated at 500°C for 75 hr. It is seen that in the case of the
agitated samples Xe segregation was unaffected but I separation was
appreciably reduced. However, the great bulk of the I was still found on
the outer layer of the Bi.
Besides these experiments, another series was carried out in which the
bismuth, containing uranium, was molten during irradiation, so that the
xenon and 1odine had a chance to escape as soon as formed. Figure 22-2
is an example of a typical experiment. In the figure, the central dark area
is the bismuth core. The bright band is that part of the graphite into
which xenon and iodine have diffused at 500°C. This band is about 1.5 mm.,
since the picture represents a magnification of 4 times. The conditions for
this particular experiment are given in Table 22-5. The irregularities
observed in the photograph are in accordance with the heterogeneity of
graphite.
It should be noted that fission products other than iodine and xenon
may be and possibly are involved in the formation of the high-intensity
800 CHEMICAL PROCESSING [cHAP. 22
TABLE 22-5
CapsurLr Trsts with MoLTEN FUEL
1000 ppm U235 in Bi+ 350 ppm Mg + 350 ppm Zr. Irradiated for 15 days
at a flux 2 X 10*2 n/(em?2)-(sec) at 500°C. Graphite G capsule
Xe!33 concentration in graphite about 1 X 10'*® atoms/g of graphite
Xel33 7 " bulk 7 3% 10° atoms/g of Bi
I3 " " graphite 7 5 X 1013 atoms/g of graphite
[131 ”? ” bulk 73 x 10 atoms/g of Bi
regions. The penetrations in the graphite appear to be due to radioactive
gases exclusively.
The results of all these experiments show that I and Xe concentrate
very heavily on surfaces in contact with the U-Bi fuel. There is evidence
that Xe and radioactive gases penetrate the graphite and are immobilized
therein. This may present a very serious problem in keeping the LMFR.
fission-product poisoning to the low levels required for economic breeding.
The reported experiments, however, have been limited by the available
neutron flux of the BNL pile to concentration levels about 1/1000 those
anticipated in an LMFR breeder. Extrapolation of the present results to
the LMFR levels is not justified, since it is conceivable that because of
saturation effects the concentrations at the interfaces may not increase
proportionately. However, the penetration of Xe in the graphite, as con-
trasted to its accumulation at interfaces, is a potentially serious problem
because of the large surfaces available inside the graphite.
The results of these experiments clearly indicate that the removal of the
FPV’s is not a simple degassing operation. An increased research program
is under way to learn more about the release and movement of the FPV’s
in both the reactor core and in the fuel streams. While degassing equipment
designed to afford a large fluid surface for escape of the gases will probably
be the best kind of equipment, the volatiles may very well never arrive at
the degasser at all. Instead, they may adhere to the graphite walls and to
the steel walls. Operation of the LMFR Experiment No. I should give
extremely valuable information on this particular question.
22-2.3 Design of equipment for FPV removal. In the LMFR, the fuel
would flow continuously through several parallel loops to external heat
exchangers for cooling. Degassing equipment would, in all probability, be
located in each of these loops. For a 500-Mw reactor, if all heat-exchange
22--3] FUSED CHLORIDE SALT PROCESS 801
streams were processed continuously, the fraction of FPV in the fuel re-
moved per pass would only be about 0.004. Since the solubilities of Kr
and Xe in B increase with temperature, the degassing equipment should
preferably be located in the coldest part of the system, but since the fuel
flow through the reactor is upward, and since the degassers must be located
at the top of the system because of hydrostatic pressure, it 1s not very
practical to locate them at the coldest point.
The main objective would be to prevent excessive amounts of Xe from
being adsorbed on, or absorbed in, the graphite moderator. To achieve
this, two conditions are necessary: first, the relative amount of I settling
on the graphite must be kept low, and second, the degassers must be very
efficient. The problem is not so much one of desorbing Xe from a Bi solu-
tion as it is one of controlling the accumulation of I and Xe on unwetted
surfaces. To minimize I buildup on the graphite, the fuel velocity in the
core should be as high as practical and there should be solid surfaces
located somewhere between the core and the degassers to collect 1.
On the basis of present knowledge, the degassers should be so designed
that a large interfacial area is provided and that the liquid metal surface
1~ ax turbulent as possible. Theoretically, a degasser should work with good
efficiency. A theoretical analysis by McMillan (BNI.-353) showed that
xenon has a tremendous tendency to concentrate on liquid bismuth sur-
faces. For a spherical volume, the number of xenon atoms on the surface
wax estimated to be about 108 times the number dissolved in bismuth at
300°C. At 500°C this ratio came close to 10°.
A sieve-plate column, in which the fuel descends in fine streams, would
be <uch a degasser. It is felt that sparging of an inert gas into the fuel 1s
not necessary to promote gas desorption, since Xe is so insoluble. However,
depending on the gas pressure in the degasser, the use of an inert carrier gas
may be desirable. The effluent fission gases would be collected in refriger-
ated charcoal beds.
22-3. Fusep CHLORIDE SALT PRoCESS
In processing the molten bismuth for the removal of fission-product
poi~ons, the ideal process would be a pyrometallurgical one operating at
substantially the same temperature as the fuel. Furthermore, this process
should either leave the uranium fuel in the bismuth or treat it in such a
manner that it is relatively easy to recharge it as a metal into the bismuth
stream for reuse. The LMFR thus offers an excellent opportunity for the
application of pyrometallurgical chemical reprocessing methods. From a
procedural point of view, such methods should inherently be cheaper than
presently known aqueous processing methods. It will be necessary, however,
802 CHEMICAL PROCESSING [cHaP, 22
to await an economic comparison of the aqueous and pyrometallurgical
processes before one is finally chosen for use with an LMFR.
However, since the LMFR offers such an excellent opportunity for the
application of cheap pyrometallurgical processing, this path has been
explored quite extensively. In this section a fused chloride salt process
for the removal of fission poisons is deseribed. In following sections a
fluoride volatility process and a noble fission product removal process are
described.
22-3.1 Equilibrium distribution. Chemistry. The FPS group consists of
the lanthanides and the elements in groups IA, ITA, and IITA of the Periodic
Table. Within this group the lanthanides account for about 94% of the
total poisoning effect of the FPS elements. In the case of a typical 500-Mw
reactor [1] the concentration of FPS elements in the bismuth amounts to
about 17 ppm. To reduce this concentration to acceptable levels, a process
has been developed whereby the FPS elements are oxidized by and then
extracted into a fused salt.
Following the original suggestion by Winsche that fission products
might be extractable from a liquid U-Bi fuel by molten salts in a manner
similar to solvent extraction, experiments were conducted by Bareis using
the LiCI-KCI eutectic and lanthanide-bismuth alloys [6]. If the mechan-
ism was indeed one of liquid-liquid extraction, then the lanthanide distribu-
tion should follow a simple distribution law and as such be independent of
total concentration. Fxperimentally, this was not the case, and it was
subsequently shown by Wiswall [7,8] and later independently by Cubic-
ciotti [9] that the results could be explained by assuming that a chemical
reaction had occurred as follows:
3LiCl(salt) + LEL(BU 2 L&Cl;; (salt) + §3Li(Bi). (22—1)
I'rom the free energies of formation of the halides involved (Table 22-6)
we may calculate AF® =+ 33.6 keal for Eq. (22-1). From this and the
relationship AF®=—RT In K¢, the equilibrium constant, K., is found
to be 3.2 X 10719, Obviously, the equilibrium will be displaced far to the
left. However, if we assume an initial La concentration in the bismuth
equal to 17 ppm, equal volumes of eutectic (KCI considered here as inert)
and bismuth, and that activities are equal to mole fractions, then the ratio
of moles of lanthanum in the salt to moles of lanthanum in the bismuth at
equilibrium will be 146. Essentially, therefore, all the lanthanum will be
transferred to the salt phase.
On the other hand, for the analogous reaction with uranium:
3LiC1+ U === UCl; + 3Li (22-2)
22-3] FUSED CHLORIDE SALT PROCESS 803
TaBLE 22-06
AF or CrrTaIN Havipus aT 773°K [10]
Compound Free energy of formation F,
‘ keal/atom Cl
Kl 88.6
SmCls 84.1
LiCl 82.6
Na(Cl 81.4
CeCls 69.8
NdClg 67 .4
UCl3 57.5
the standard free energy change is +75.3 keal, and Keq = 5.2 X 1022
At equilibrium, assuming the initial uranium concentration in the bis-
muth = 1000 ppm, the ratio of the mole fraction of U in salt to the mole
fraction of U in Bi will be equal to 6.8 X 107%. Thus, in principle, a selec-
tive oxidation of the lanthanides may be achieved in the presence of
uranium. Of course, the assumption that activities are equal to mole
fractions is only an approximation.
Ternary salt. As a consequence of these reactions, lithium metal builds
up in the bismuth phase and, in view of its high thermal neutron cross
section, replacement of the lanthanide by lithium offers no advantage in
terms of neutron economy.
Therefore another low-melting salt, the ternary eutectic of MgCla(50
mole 77, KCI (209,), and NaCl (30%,) (M 396°C) was investigated.
In this system, the free energy of formation of MgClz is intermediate
hetween those of the lanthanide chlorides on one hand and uranium
trichloride on the other and a satisfactory, although not complete, separa-
tion should be achieved.* Furthermore, the low neutron cross section of
Mg iz more favorable than that of lithium, and a low concentration of Mg
in the fuel (250 ppm) appears to be necessary in order to minimize cor-
rosion and mass transfer in the steel equipment. The magnesium con-
centration in the bismuth will therefore control the extent of the reaction:
*The stability of NaCl and KC1 is so much greater than that of MgCly that their
contribution to the oxidizing potential of the salt may be neglected. However, they
do exert an influence upon the activity coefficient of MgClo.
804 CHEMICAL PROCESSING [cuap, 22
BNIgCIQ(Sglt) + 2La(Bi) —.<_..—>' 2L‘d013(3a1t,) + 31\’1%‘(31), AFV = —5H8.2 kcal,
(22-3)
gngCIQ(Salt) —I— 2U (Bi} <—— ZUClg(qam "Jr- ?\Ig_,(Bg, AFO +2-) 2 kCcll
(22 4)
but will not influence the degree of separation which may be achieved.
Thermodynamics of FPS transfer and distribution data. The equilibrium
constant for reaction (22-3), in which lanthanum is taken as being repre-
sentative of lanthanides in the 43 oxidation state, is given by
2 3
A1aCl; AMg
Ke — . 0=
1 ata dliee, (22-5)
Expressed in terms of mole fractions, liq. (22-5) becomes
3 0
Keq — X%aCh XIVIQ; . (f[?:Ci?)Q (.fMg)B . (2276)
XTa Xect, (fla)? (Frreon)®
In the above, a = thermodynamic activity, X = mole fraction, and f and
f* are activity coeflicients. f* is the limiting activity coefficient at infinite
dilution, which is assumed to he independent of concentration at the
concentrations encountered in this investigation. It is equivalent to the
Henry’s law constant [11}.
Solved for the experimentally detesminable quantity Xyaci,/Xrta., Eq.
(22-6) becomes
-3 -
Xiacl, _ (K g X MgClg)] /2 , (22-7)
XLa Kf X?I)\Ig
where
_ (fTact,)? (ff’lg)‘?'
(T (aecty)?
In logarithmic form, (22-7) may be written
XLa.Cl; - 3 L Keq(XNIgClz)B .
IOg X = 5 10g Xl\{g + E 105J “‘7}—-——1 (22 8)
whereupon, a plot of log Xra.ci,/X1. versus log Xy, should result in a
straight line of slope =-—3,2. Figure 22-3 is a plot for most of the I'PS,
uranium, and zirconium based on the best experimental data. In the
case of La, the best line has a slope of —3,/2. T'rom the position of the line,
the constant term of Eq. (22-8) may be calculated by
22-3] FUSED CHLORIDE SALT PROCESS 805
emf, Volts vs Zn/ZnClg(.~) //
~0.40 —0.50 ©@=0001
1000 1 v | 1 1 l T T 7 i T T 7T
~ Sm La 3
500 |- 3
200 b .
100
T [Illlll
1 llijlll
wn
3
1
201 U
I I!IIIII
L lllnll
k, (wt. % insalt) / (wt. % in bismuth)
o
2 N\ Zr
B N\ i
N\
e N\ ]
- N\ E
- AN ]
. \\ N\ .
| \ Nz
0.2+ \\ -
\U
01— \ — o
- N3 Fig. 22-3. Distribution of solutes
ost o Lianl ] ] ] L 1] 0 \/ - - 1-V
005 L 250\ = between MgCla-NaCl-KCl and Bi-Mg.
Mg in Bi, ppm
g KGC} (XMECIQ)S .
B {constant) = 1 lo 7
S
5 (22-9)
[xperimental values of these constants are given in Table 22-7.
Comparison of theory and expertment. In order to compare theory with
experiment, Ko, Xwecn, and the activity coeflicients of the pertinent
<ubstances in each phase must be known. K, is easily calculated from
the AF#* for the appropriate reaction by means of the relation AF®
— —RT In Koy Xvger, may be considered essentially constant and equal
to (1.3, since MgCly is present in the salt phase in large excess over the other
reactants and its concentration changes only very slightly during the
reaction. An exact caleulation of K; is not possible at this time, owing to
the paucity of information regarding activity coefficients in fused salts
aud in Hquid bismuth. However, in one case, that of cerium, it is possible
1o extimate K, from measured activity coefficients if one assumption is
allowed. Recently Egan [12,15] has measured the partial molar free energy
of mixing, AF, of magnesium in bismuth and cerium in bismuth by galvanic
cell mothods. From AFy, and AFq,, it was possible to calculate fug and
f%. the activity coefficients at infinite dilution, in bismuth at 500°C.
These values are estimated to be f{,=2X 1072 and f& =3 X 1071
TaBLE 22-7
VALUEs oF B (CONSTANT)
Reaction —AF0
2La + 3MgClo =2 2LaCls + 3Mg 58.2
2Ca + 3MgCls === 2CeCl3 + 3Mg 48 .6
INd + 3MgCly == 2NdCl, + 3Mg 342
Sm + MgCle === SmCls + Mg 44 8
2U + 3MgCly, === 2UCl3 + 3Mg —25.2
Keqg —B — B’ K =
2.84 x 1016 3.2924 — 1.36 X 1022 4 x 1018
5.49 x 1013 3.9586 — 5.67 x 1020 2x 1015
4 66 x 109 3. 8873 — 3.49 x 1016 2x 10718
4.62 x 102 — 1.8097 1.49 x 1014 4 X 10713
7.52x 1078 — — — —
908
DNISSHI0 d "TVIINAHD
0% "dVHD]
22-3] FUSED CHLORIDE SALT PROCESS 807
(Table 22-8). Neil [13] by similar galvanic cell techniques, has meas-
ured the activity coefficient of MgCls in the ternary salt eutectic
MeCle-KCI-NaCl at 500°. The best value to date is faec, = 0.34. If it
is assumed that &, = 0.1 in the ternary salt (and this value appears
reasonable), then K, for cerium is given by
_ (&) (fMe)® _ (1071)*(2 X 107%)°
= _ = =923 X 108,
(P& (Tmcn)® — (3 X 10 #)2(0.31)7 0
K;
The experimental value of K; 5.6 X 102, leads to a value of 2 X 1071®
for f&c,. The agreement is considered satisfactory, in view of the ex-
ponential character of the equations and the uncertainties in the available
data.
For example, the entire difference between the experimental value and
calculated value of K; may be reconciled if one assumes an error of
1.4 keal ‘atom Cl in the AF of formation of CeCls. Such an error is well
within the limits with which the standard free energies of formation are
known at these temperatures. The estimated activity coeflicients of
metals in bismuth may also be in error by as much as a factor of 2 to 3.
The experimental values of the constant Br, and Bng (Table 22-7)
mayv be used to caleulate the activity coeffictents of lanthanum and
neodvmium in the bismuth if it is assumed, as in the case of cerium, that
i, = fRac, = 0.1. The values so obtained, ffa=4 X 107 and fRq
=2 x 10713 are quite low, and are in general agreement with the
measured f&,.
In the case of samarium, SmCls is thermodynamically more stable
than SmClz by 14.6 keal/atom of Cl at 500°C, and hence the equilibrium
reaction 1s
Sm i) + MgClagay === SmCla gy + Mgmi). (22-10)
In a manner analogous to the treatment of the trivalent lanthanides, we
obtain
lOgg{%@E:_IOg Xmg+ B, (22-11)
Sm
where
Ke XM Cl ’ féOmCl fi?I
B =1 d B d K= s 2=2r T8,
Ky an I & f MOl
808 CHEMICAL PROCESSING [chap. 22
TaBLE 22-8
Activity COEFFICIENTS AT
INFINITE DIiLvuTIiON
System Temperature, °C fir
Ce-Bi1 200 3 X 1014
Mg Bi 500 2 % 103
U-Bi1 500 1 x 1073
Li-Bi 450 1x 10753
Na—-Bi 500 8.5x 1075
7Zr—Bi 700 77X 1074
Equation (22-11) prediets that a plot of log Xsmen/Xsm versus log X
should yield a straight line of slope —1. The curve is shown in Fig. 22-3
and the line is drawn with a slope of —1. This line yields the value of B’
given in Table 22-7. With the assumption that f&.c, = 0.1, the estimated
activity coefficient at infinite dilution of samarium in bismuth is
JE8n=3 X 1078
The validity of Eq. (22-6) is dependent upon the assumption that side
reactions, such as the oxidation of bismuth by the salt, are negligible.
Since AFC for these reactions are large positive numbers, it is reasonable
to consider bismuth as inert in this respect. Bismuth, of course, interacts