HOME HELP
L,
ORNL-TM-2490
C o n t r a c t No. W-7405-eng-26 METALS AM> CERAMICS DIVISION
COMPATIBILITY OF HASTELLOY NaBFk-NaF-KBF4
N AND CROLOY 9 M W I T H
(904-6 m o l e
$1
FLUOROBORATE SALT
J. W. K o g e r and A. P. Litman
LEGAL NOTICE
*c
P 3
Thla mwrt
DovernmMt mpollllored work. Neither the Unlted h i e m , wr the CommlasIon. nor uy perm .CUI.% on behalf of the Commlaslon: A. Makes .epWuMtyor represent8tim,exPressedor Implled.with respect to the sccum y . completenese. or ~ ~ I u l n eof s sthe Wormatlon contained la thla report, or that the w e of my Wormatlo% aprmratus, mstbod. or pmcess disclosed In thls mport m a y not infringe prhtnly owned r i g h or B. h m u n e n m y IllbiUueswith respect to the we of. or for &mZea readfmm the nsa of uy Information. apparatus. method. or +ess dl.cl0sed h thla r e m A. uaed tu the h e . "pernon actbg 011 behal~ of tbe &mmiaaion" includes uy emp l o y ~or conmetor of the Commlsslon. or employee ol much conmetor. to the extent that much employee or contractor of the Commlsaion, or employee of much contractor p p r e s . j dls~mlnatas.or provides sccess to. my informath puauaat to his empiopeut or contract 4 wlth the Commlmdon. or his employment with Neb contractor. Y I prepnred ~ as u1 scEOIult'of
:
--
-.
APRIL 1969
.e
OAK RIDGE NATIONAL LABORATORY Oak R i d g e , Tennessee c
operated by UNION CARBIDE CORPORATION for the U. S. ATOMIC ENERGY COMMISSION
ti
iii
CONTENTS
Page
........................... Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . Experimental Procedure . . . . . . . . . . . . . . . . . . . . . . Materials Section and Fabrication . . . . . . . . . . . S d t Preparation . . . . . . . . . . . . . . . . . . . . Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Abstract..
Results
............................. NCL-10 (Hastelloy N) . . . . . . . . . . . . . . . . . . NCL-12 (Croloy 9M) . . . . . . . . . . . . . . . . . . . .......................... Thermodynamics of System Corrosion . . . . . . . . . . . Kinetics of System Corrosion . . . . . . . . . . . . . . S a l t Purification . . . . . . . . . . . . . . . . . . .
Discussion..
.
........................... Recommendations . . . . . . . . . . . . . . . . . . . . . . . . . Acknowledgments . . . . . . . . . . . . . . . . . . . . . . . . . Conclusions
1 1
3 5 5
7 9 9
19 26 31 33 36
37 37
38
b
'
COMPATIBILITY OF HASTELLOY N AND CROLOY 9M WITH NaBF4-NaF-KBF4 (90-4-6 mole
*
$1
FLUOROBORATE SALT
J. W. Kbger and A. P. Litman
ABSTRACT
The compatibility of a relatively impure (> 3000 ppm impurities ) fluoroborate salt, NaBF4-NaF-KBF4 (90-4-6 mole $1, with Hastelloy N and Croloy 9M was evaluated i n natural c i r culation loops operating a t a maximum temgerature of 605째C with a temperature difference of 145째C. The Croloy 9Mloop (EL-12) was completely plugged a f t e r ,1440 h r of operation and the Hastelloy N l o (NCL-10) was three-quarters plugged a f t e r 8760 h r (one year of .operation. All major a3loying elements of the container materials mass transferred during operation as the r e s u l t of nonselective attack by virtue of the i n i t i a l oxygen and water contamination of the salt. Saturation.concentrations of 700 ppm Fe and 470 ppm C r were determined f o r the fluoroborate salt a t 46OOC. The mechanism of corrosion of the system i s as follows. I n i t i a l l y , metal fluoride compounds t h a t a r e soluble i n the salt are formed i n the hot leg. "he reverse reaction occurs i n the cold l e g and causes the metal t o de o s i t and t o diffuse i n t o the cold leg. This continues u n t i l 1) an ecpilibrium concentration of one o r more m e t a l fluorides is reached i n the salt at the coldl e g temperature and these compounds start depositing (e.g., NCL-10) or, (2) the equilibrium constant of the reaction changes so much with temperature t h a t the pure metal i s deposited (e.g., NCL-12).
9
L
c
-4 % c
e
ODUCTION
Nuclear reactors t h a t use molten fluorides as fhels a r e under development f o r the dual purpose of power production and thorium conversi0n.l
Heat generated i n the core region of such a molten-dalt
L l i
-&
breeder reactor is transferred from the fuel-containing fluoride s a l t t o a secondary cool
rcuit of fluoride salt with
Q
hJ
M ' SR Program Semiann. Progr. Rept. Feb. 29, 1968, ORNL-4254.
'
2
ai
then dissipates the heat t o stem2 In the h l t e n - S a l t Reactor Experiment
(MSRE), the nickel-base alloy Hastelloy N has proved t o be an effective container m a t e r i a f o r the fluoride salt that contains the fuel and for the LiF-BeF2 diluent.
any potential fissile2 (containing U F ~ f e r t i l e 2 (containing ~ o r combination' (containing both UF4 and ThF4) salts proposed f o r the
h ), ~
MSBR have been or are being tested f o r t h e i r compatibility w i t h
Hastelloy N and other container materials.
"he choice of a salt for
the secondary coolant, however, remains open.
Test programs have only
considered coolant salts l i k e NaF-ZrF4 and, recently, IXF-BeF;!.
While
these salts have demonstrated excellent ccanpatibilitywith Hastelloy N, there is need f o r cheaper fluoride mixtures t h a t m e l t a t lower tempera-
On the basis of l o w cost (approximately 504/lb) and a r e l a t i v e l y l o w melting point (about 4OO0C, necessary f o r transferring heat t o supertures.
c r i t i c a l steam), fluoroborate s a l t s
- especially NaEF4 - w i t h
small
additions of NaF and/or KEP4 have recently become of interest as secondary coolants.
L i t t l e i s known, however, about the corrosion behavior
of these salts. The space diagram of the ternary NaF-NaRFc-KBFk system (Fig. 1 ) shows t h a t the salt mixture under consideration l i e s very near the NaBF4 corner and has a m e l t i n g point close t o 390째C.
Note t h a t oxygen impu-
rities that form BF3OH-c0mpounds significantly lower the melting point of the mixture below t h a t Shawn by the diagram.
The vapor pressure of
fluoroborate salts, especially NaBF4, i s higher than t h a t of other fluoride saltsY3because i n the temperature range of interest the sodium fluoroborate maintains such an equilibriumwith i t s components t h a t a significant amount of boron t r i f l u o r i d e gas i s present i n the system: NaBF'4 'NaF
+ BF3(g)
.
(1)
2P. R. Kasten, E. S. Bettis, and R. C- Robertson, Design Studies of 1000-W(e) h l t e n Salt Breeder Reactors, ORNL-3996 (August 1966). 3H. S. Booth and D. R. Martin, Boron Trifluoride and Its Derivatives, Wiley, New York, 1949.
4
3 ORNL-OWG NaF*K6F4
(90-4-6
SE-5560R
mole %I
KBF.
61
NaF (999)
\/
I ?. 1
E
v
/vi
v
V 720
V
,I
(6%P,
..
Fig. 1. Little
v/
Space Diagram of the NaFLNaBFheKBFb-KP System
is known about the corrosion behavior of the BF3 gas.
A few corro-
sfon experiments ha&,been,a, run with very dry BF3 gas,4 and little appreciable attack':was found up to 200°C on metals such as brass, stainless steel, nickei, Monel, mild-steel, and ,manyothers. $his report describes-the first comprehensive study of the compatibility of a relatively impure fluoroborate salt with Rastelloy N and‘Croloy.9M alloys. The experiments were designed to yield information on temperature gradient mass transfer, the major form of corrosion in fluoride salt systeks. ~Twoloops were operated with NaEIlQ-NaF-KBF4 (90-4-6 mole $1 salt at a maximumtemperature of 605°C with a.temperature difference of 145°C to obtain the data presented. These*temperatures match those proposed for fluoroborate salts in a1 molten,,salt breeder '. reactor. I EXPERIMENTALPRCCEDURE !Thenatural-circulation loops for this program were'of the type shown in Hg. 2. Flow results from the difference in density of the 4F. Rudswell, J. S. Nairn, and K. L. Wilkinson, J. Appl. Chem &, 333 (1961).
Fig. 2.
C
Natural. Circulation Loops in Test Stands.
* \ A rn
5
bd
salt i n the hot and cold portions of the loop. of salt f l o w i n the
We estimated the velocity
loops t o be 7 f't/min.
x
Materials Section and Fabrication 1
The Croloy 9M material was from Babcock 8~ Wilcox Company heat 18760 and was vapor blasted before fabrication t o remove oxides. NCL-12,
The loop,
was fabricated fYom 0.750-in. -OD tubing with a w a l l thickness of
0.109 in
The material was TIGwelded and inspected t o meet existing
internal standards.
The welded areas were torch annealed before and
a f t e r welding. The Hastelloy N material was f'rom Union Carbide Corporation, Materials Systems Division heat 5096.
The loop, NCL-10, was fabricated
from 0.672-in. -OD tubing with a w a l l thickness of 0.062 in.
, T I G welded
and inspected t o meet the same standards as those required for the Croloy 9M material. The compositions of both alloys are given i n Table 1. Table 1. Chemical Composition of Alloy Test Materials c
$1 Mns
Composition (wt
Hastello N (NCL-107
.Fe
Ni
Cr
bb
70.8
7.47
15.59
C
4.01
0.07
0.54
0.005
89.00
0.09
0.48
0.012
P
Si
0. a 0.010
0.47
S a l t Preparation
Reactor Chemistry Division a t ORNL. P
~
with a fluoroborate salt,
This was t h e i r first experience
they prepared it by techniques established
L
>.
f o r other fluoride salt
raw materials - r e l a t i v e l y impure NaBFi,
ORNL-3626, p. 146.
6 NaF, and
KEP4
(90-4-6 mole
$1
(Table 2) -were loaded into a container
W
l i n e d w i t h nickel, which w a s then evacuated and purged several times with helium.
Then, the materials were melted and heated t o 400째C under
a helium atmosphere.
N e x t , the l i q u i d was sparged with helium,
?
..
Since I
t h i s caused a large increase in pressure, the reactor vessel was vented. Large quantities of BF3, which had caused the increase in pressure, were then released.
Later steps included sparges with a mixture of hydrogen
fluoride and hydrogen for several days at 550째C t o remove oxides and a The salt
sparge with hydrogen t o remove structural metal impurities.
was then transferred t o a f i l l tank made of Hastelloy N i n preparation for f i l l i n g the loop. The chemical analysis (Table 3) of the prepared salt disclosed two important compositional changes germane t o t h i s t e s t series:
(1) a
significant loss of BF3 during preparation, and (2) a high content of oxygen and water. Since l i t t l e was k n m about the corrosive behavior of t h i s salt o r the effect of impurities and because information on i t s compatibility with the container alloys was needed quickly, w e decided t o use it as prepared. Table 2.
Composition of S a l t Mixture Before Purification
&uantities Loaded in Container Compound DF4
NaBF4 NaF
5.88
6.85
90.20
91.61
3.92
1.53
Chemical Analysis Element 2 -10
K
Na
.
20.00
B
9.60
F
68.30
bd
7
e,
Table 3. -~
Chemic82 Analysis of Salt Before Fill
~
Element
Content (wt
$1
K
2.20
Na
25.80
B
9.65
F
60.40
Ni
< 5&
Cr
54&
Fe
28&
S
6' 3O0Oa
02
900, 21ooa
H20
8PeLlrts per million. OPERATIONS The hot portion of each loop was heated by s e t s of clamshell heaters, with the input power controlled by silicon controlled r e c t i f i e r s .(SCR units) and the temperature controlled by a Leeds and Northrup Speedomax H Series 60 type C. A. T. (current proportioning) controller.
The loop tem-
peratures were measured by Chromel-P vs Alumel thermocouples t h a t were spot welded to the outside of the tubing, covered by a layer of Quartz
tape, and then covered with stainless s t e e l shim stock. Before each loop and heated t o 150째C unde
I
p
a t
u
i t h s a l t , it was degreased with acetone t o remove any moisture i n the system.
8 We checked for leaks with a helium mass spectrometer leak detector while the interior of the loop was evacuated t o < 5
X
torr.
All l i n e s
from the f i l l tank t o the loop that were exposed t o the fluoroborate
I
salt were of the'same material as the loop and were cleaned and tested ~
i n the same manner as the loop.
A l l temporary l i n e connections were
II
L
made w i t h stainless s t e e l compression f i t t i n g s . The loops were f i l l e d by heating the loop, the salt pot, and a l l connecting l i n e s t o a minirmlm of 530째C and applying helium pressure t o the salt pot t o force the salt into the loop.
Air was continuously blown on the freeze valves leading t o the dump and flush tanks t o provide a positive salt seal. Tubular e l e c t r i c heaters controlled by variable autotransformers fbrnished the heat t o the cold-leg portions.
Once
the loop was f i l l e d the heaters were turned off and the insulation was
removed t o obtain the proper temperature difference by exposing portions of the cold leg t o ambient a i r . The first charge of salt was dumped a f t e r 24 h r i n the loops a t the
maximum operating temperature with some circulation and l i t t l e temperature gradient. This flush remved surface oxides and other impurities that could have been l e f t in the loops. The loops were then r e f i l l e d with new salt and put into operation. A helium cover gas under slight positive pressure (about 5 psig) was maintained over the salt i n the loops during operation.
l t
I'
Each loop was operated a t a maximum temperature
of 605째C and with a temperature difference of 145째C.
A temperature pro-
f i l e around the loops i s sham around the schematic of the loop i n Fig. 3. During circulation each loop contained about 920 g of salt that contacted 1200 cm2 of surface and traveled 254 cm around the loop. Temperature excursions indicated a f l o w stoppage in NCL-12 (Croloy 9M) after 1440 hr.
*
A t t e m p t s t o drain the loop were &xsuccess-
f'ul, and the loop was' allowed t o cool w i t h the test salt in place. In NCL-10 (Hastelloy N), a significant increase of temperature i n the hot l e g accompanied by a simultaneous temperature decrease i n the cold leg occurred a f t e r 8335 h r of operation.
A perturbation of t h i s type indi-
cates a disruption in salt flow and can indicate plugging.
This tem-
perature cycle ceased after 1hr, and no f'urther incidents occurred
4
1 l -
9 ORNL-DWG 68-4t180
SURGE TANK ~
f 10.C
\
CLAMSHELL HEATERS
i+-INSULATION
I I
I
jI II
0.C
DUMP TANK
Fig. 3.
Schematic of MSW Natural Circulation Loop.
during the l i f e of the loop.
The loop was shut dawn a f t e r 8760 h r (1 year), and the salt w a s drained'into a dump tank i n a normal manner. RESULTS
Analyses of loop components and salt were made by standard chemich analysis, metallographic examination, and electron microprobe analysis. The results are discussed beluw. c
NCL-10 (Hastelloy N) Visual.
s
w
- A p a r t i a l plug i n the lower part of the cold l e g
(Fig. 4 )
closed approximately 75$ of the cross-sectional area of the pipe.
Analysis
10 -.
. TUBE WALL
PLUG
L
Fig. 4. Plug Formed i n NCL-10 (Hastelloy N) Containing NaBF4-NaF-KBF4 (90-4-6 mole $1 After 8760 h r a t a Maximum Temperature of 605째C and Temperature Difference of 145째C. &. Reduced 40%.
B
shared this emerald-green plug t o be single crystals of Na3CrF6 (ref. 6 ) . Smaller amounts of two complex iron fluorides, Na3FeF6 and NaFeF4, were a l s o identified in the cold leg. Chemical.
- The analysis of
the salt cake (Fig. 5) collected from
the dump tank of NCL-10 i s given in Table 4. The concentrations of nickel, molybdenum, iron, and chromium i n t h i s s a l t were higher than those of the salt before t e s t .
The average chromium concentrationwas
470 ppm. Due t o cooling, nickel was segregated i n the top and bottom portions
of the cake, reaching 11.15 and 4.47 w t $ i n these portions, respectively. The analysis indicated that the water content of the salt 6MSR Program Semiann. Progr. Rept., AM.
- 400 t o 900 ppm
31, 1967, ORNL-4191, p. 228.
-4
t
11
td
Fig. 5.
II
Table 4.
Drain S a l t Cake From NCL-10 (Hastelloy N)
Impurity Analysis:
.
(90-4-6 mole
'$1
0
S
NaBFd-NaF-KEiFh Analysis (ppm)
5
Ni
Before t e s t
87
Cr
83
Ivb
7
Fe
146 1400 3000 4850
H20
400 2,6 900
After test
Top slag
E L -15'
Center layer
90
Bottom layer
-.-
4.47a
%eight percent.
1.35a 210 160 1500 7300
4200 1200 1800 5 1750 270 3540 1.300 2, < 5 3120 1500 3550 2800 3660
< 5,19
12
before t e s t -increased t o 1300 t o 2800 ppm.
The oxygen analyses showed
much scatter, but we believe t h a t the oxygen content also increased. Presumably these increases are due not t o air inleakage but t o other factors discussed l a t e r i n t h i s report. The crossover l i n e t o the cold leg, the cold leg, and the crossover
r t
.
l i n e t o the hot l e g all showed slight increases i n wal+ thickness due t o deposition of complex surface layers (Fig. 6).
Chemical analysis of the
layers disclosed that they were primarily metallic nickel (60 t o 90 w t $) and molybd&mm.
A sma.ll quantity of iron was present i n proximity t o the
base metal, but chromium was conspicuously absent. Metallurgical.
- Micrometer measurements of
the hot leg of the loop
disclosed 1 t o 2 m i l s of metal l o s s and s l i g h t surface roughening. Metallographic examination of an area fromthe hottest section (605OC), however, showed a smooth surface w i t h an occasional penetration along a grain boundary (Fig. 7 ) .
Microprobe traces7 of this hottest
section for all the alloying elements showed no compositional gradients. The chromium trace f o r t h i s section i s given i n Fig. 8 .
These results
indicate a general dissolutive attack in the hot-leg section.
An area a t the entry of the cold l e g (520OC) showed a duplex surface structure, and the areas numbered i n Fig. 9 were analyzed w i t h the microprobe f o r the various elements (Fig. 10). is quite high in nickel
- trp t o 87 w t $.
The outermost layer, area 1,
We believe t h i s i s most l i k e l y
a region where nickel deposited during the t e s t . taining essentially only molybdenum and nickel.
Area 2 is a region conClose t o the original
metal surface there is an increase in nickel, a smaller increase i n molybdenum, and l i t t l e change in chromium and iron.
Note that w i t h an
increase i n nickel and molybdenum metal the concentration of chromium and iron would show a decrease even though there were no change i n the actual amounts. Figure ll, a photomicrograph of the coldest section NCL-10 (46OOC)
shows a spongy deposit on the surface and a loosely adherent corrosion product beyond t h i s region.
A t higher magnifications,
5
it was seen t h a t
the t i g h t l y attached spongy deposit varied in thickness from 0 t o 6 pm
7Data not corrected f o r absorption, secondary fluorescence o r atomic number effects.
I
i
ORNL-DWG 67-9342R
,’ ,’
I I
0.007 inches
I
32.5 in.
I
0.007 inches
LOCATION OF Na, Cr F6 PLUG,
NCL 10 SALT: NaBF$NaF-KBF4 (90.4-6 mole %) . TEMPERATURE:605’C,AT= 145”C,TIME = 8760 hr
Fig. 6.
&face
Layers in NCL-10 (Hastelloy N) After 8760 hr Operation.
14
c
P i g . 7. Hastelloy N Hot-Leg Section E L - 1 0 (605째C) s h m a t Different Magnifications After 8760 h r i n Fluoroborate S a l t . Etchant: Glyceria Regia.
W
ORNL-DWG
-
"
I
-
n
0
W
68- 9658
n
0
I TRACES OF Ni,Fe, AND Mo SHOWED NO GRADIENT
I
I I
3
2
AA
I
10
20 DISTANCE ( p )
Chromium i n Hot Leg (605째C) of NCL-10 Fluoroborate Salt.
'\
30
ast e u o y N)
40
After 8760 h r i n
16
U P
Fig. 9. Entry t o Cold Leg (520째C) of NCL-10 (Hastelloy N) Operated for 8760 h r i n Fluoroborate Salt. Etchant: Glyceria Regia. (a) 500x. (b) Numbered areas were anaLyzed by microprobe. 2000X.
bd
E
.'
91
W
I
c
ORNL-DWG 68-9659
Ni
-.e --.-.\
80
I
-
Mo
-0-0-
-*-e-.--.-.-
-.-e--t-.-.e-
Fe
0 0
io
20
30
40
DISTANCE ( p )
Fig. 10. Penetration Curve of Constituents of Hastelloy N a t Cold-Leg Entry (52OOC) of NCL-10 Operated for 8760 h r i n 3luoroborate Salt.
.
18
X
a
Fig. ll. Coldest Section ( 4 6 0 째 C ) of NCL-10 (Hastelloy N) Shown a t Different Magnifications After 8760 hr i n Fluoroborate Salt. Etchant: Glyceria Regia.
19 and that it resemble much thinner.
area seen i n the
r y t o the cold leg, although
The spongy layer i s high i n nickel, w i t h some molybdenum,
and appears, l i k e the area 1 of Fig. 9, t o have resulted f’rom nickel deposition (Fig. 1 2 ) .
There was only 63f metal i n t h i s spongy layer;
the b a l a x e was fluoride compounds.
The original surface i s high i n
nickel and molybdenum and low i n chromium and iron and is a n area where nickel and molybdenum have diff’used into the matrix.
No analysis of the
loosely adherent material was possible. The last section of the loop examined was an area a t the entrance I
Although the salt was being heated here, the temperature
t o the hot leg.
was s t i l l low enough (< 530°C) t o make t h i s an area where material was Again, a duplex layer was seen (Fig. 13) and found t o
being deposited.
be predominantly nickel, 65 t o 90$ metal and the balance fluoride com-
pounds (Fig. 14).
X-ray diff’raction analysis of the fluoride compounds
disclosed an unidentifiable crystal structure, probably a mixture of several fluoride compounds.
The surface layer had somewhat more nickel
and molybdenum than originally, and, thus, smaller concentrations of chromium and iron. E
NCL-12 (Croloy 9M)
Visual.
-
When t h i s loop was sectioned for examination, a dark
gray plug that completely f i l l e d the cross-sectional area for a v e r t i c a l distance of 1 in. was found i n the cold l e g (Fig. 15). Also, small, green crystals were see i n line, and a metallic layer w a s found against the i n s i
ing i n the cold section and i n the
salt. The thin metallic 1 inside of the tubing i loop).
2.5 mils thick was deposited on the cold-leg section (over one-half the
In some places, the material had become detached f’rom the tubfng
and was found i n the f’rozen salt (Fig. 16). 1
8
The metallic layer repre-
ss of the m t e r i a l (mostly salt) removed op. Chemical analysis revealed the layer (by mechanical means) fko t o be 90 wt 4 Fe and 10 wt $ C r metal.
sented about 4$ of the t o t
ORNL- DWG 68-9660
80
- .._.
c
Ni u
u
v
60 h
6? c
3: U
z
0 40
-
tu 0
I-
-
v)
0
a
I
2 0
SPONGY LAYER
0
20
I
I I
0 DISTANCE ( p )
Fig. 12. Penetration Curve of Constituents of Hastelloy N i n Coldest Section (460째C) of NCL-10 Operated for 8760 h r i n Fluoroborate S a l t .
c
G
I
M
m
u)
21
ti
c
i
ky
Fig. 13. Entry t o Hot Leg (530'C) of NCL-10 (Hastelloy N) Shown a t Different Magnifications After 8760 h r i n Fluoroborate S a l t . Etchant: Glyceria Regia.
22 DRNL-DWG 68-966f
I
o o-*-.-4*1-.-.
* ?I
'
0-0-0-
Ni
I 60
-f
I
65-9070 METAL I BALANCE i FLUORIDE SALT I
-
-I ~
3
d
I
41
LJ
LAYER
J
ESTIMATED ORIGINAL SURFACE
T
I
t
2
0
I 40
I
I 1 I I
P
i5 V
I
I 20
I
I
I
Fig. 14. Penetration Curve of Constituents of Hastelloy N i n HotLeg Entry (530째C) of NCL-10 Operated f o r 8760 h r i n Fluoroborate S a l t .
Fig. 15. Iron. Dendrite Plug i n Coldest Section (460째C) of NCL-12 (Croloy 9M) Operated i n Fluoroborate Salt f o r 14.40 h r a t a Maximum Tem, perature of 605째C and a Temperature Difference of 145째C.
W
23
it
6d
Fig. 16. Cross Section of Tubing of NCL-12 (Croloy 9M) Shuwing Deposited Metal Layer. Loop operated for 14-40h r i n fluoroborate salt a t a maximum erature of 605째C and a temperature difference of 145째C. Reduced 22%. Cross section of NCL-12 tubing. (b) Enlarged view of metal and salt interface. 30X.
24 The dark-gray plug located i n the coldest p a r t of the loop was come found similar crystals adhering t o speciposed of dendritic crystals. W
mens i n the hot l e g (Fig. 171, but we assume that these crystals, grming and circulating i n the salt stream, attached themselves t o the specimens
while the loop was cooling. Chemical. -Chemical analysis showed t h a t the dark-gray plug and the material on the specimens were essentially pure iron with l e s s than 1% of other elements (sham below). Elements
Content ( w t 99.00
Fe
0.03
B
Mn
< 0.05 < 0.01
Mg
0.05
Cr
<
Pb Si
0.02 0.02
cu
0.05
m
0.02
*
The results of chemical analysis of the green crystals i n the drain leg are given belm.
-
Elements
wt%
Na
10-15
B
Fe
2 4 45.9 0.058 18
Cr
12
F K
Mn
1.5
The stoichiometry of t h i s green deposit, based on t h i s analysis, color, and other factors, is roughly 2NaF-FeFa-CrF3-BF3, which corresponds t o chromium and iron fluorides mixed with the salt.
f
*
W
Fig. 17. h e Iron C tals f k o m NCL-12, Which Ope d for 1440 hr i n Fluoroborate Salt at a Maximum Temperature of 605째C and a Temperature Difference of 145째C. 1OX. Reduced 12%~. (a> Crystals adhering to specimen, and (b) c r y s t a s removed from specimen for photographing. \
26
Table 5 gives t h e composite of the salt before and a f t e r operation.
U
The significant changes i n the salt chemistry due t o t e s t axe the increases
i n the chromium and iron content from 54 t o 255 and 28 t o 700 ppm, respectively. Composition of Salt Before and After Operation i n NCL-12
Table 5.
Composition ( w t K
Na ~
B
$1 F
Composition (ppm) Cr
Ni
Fe
Mo
S
0
~~
Before Test Theoretical (calculat ed) Before F i l l
2.10
20.00
9.60
68.3
2.20
25.80
9.65
60.4
During F i l l
1.98
18.83
9.38
66.2
<
5
87
54
28
3000
83 146
1400
After Test Hot l e g
1.55
19.72
9.29
67.1
265
700
Cold l e g
1.89
20.71
9.27
67.3
255
700
< <
20
7 3000
20
< 2 3200
Metallurgical. -Metallographic examination of the hot-leg loop tubing (Fig. 18) disclosed a f a i r l y smooth surface, and micrometer measurements shared an average 2.5 mil loss fiom a nominal pipe diameter. Electron microprobe analyses were made on tubing from the hot- and cold-leg sections of NCL-12:
the hot-leg analysis (Fig. 191, consistent
with the metallographic results, shared no iron or chromium concentration gradients; the cold l e g analysis (Fig. 2 0 ) showed an increase of about
4 w t $ i n iron concentration and a decrease of about 4 w t $ i n chromium concentration ( i . e.
, an iron-rich
surface layer 1.
. DISCUSSION
The tests described are the first study of the compatibility of a
i
fluoroborate salt with container materials of interest t o molten-salt reactors.
Unfortunately, l i t t l e was known at the time of the t e s t about
the purification of the salt o r the characteristics of mass transfer i n
*
LJ
27
T
8
FA&. 18. Hot Leg (605'C) of NCL-12 (Croloy 9M), Which Operate for 1440 h r i n Fluoroborate S a l t . Etchant: Picric acid, hydrochloric acid, and ethyl alcohol.
ORNL-DWG 60-9663 I
I
Fe
o
-6
0
90
- 86 e
-
-OO o
0
w
0
0
D
"
O
I
I
0
-
0
0 0 0
-
O
0 0
1
F
i
Fig. 19. Penetration Curve f o r Iron and Chromium i n the Hot Leg Which Operated for 1440 h r i n Fluoroborate (605째C) of NCL-12 (Crolo
salt.
CJ
,
28
b;
94 0
-t9 90
-
o*
v -
c
3
2
86
0 42
k t (L 8
z
8
0
'
a .
0
0
..
--..-..a-.
t-
z
o u u0
0 0
0
0
Y
U
0
n
~
"
0
n
o w
0
c,
0 0
0 ' 0 "
Fe
0
TO-.'.
.a.
i
. .
.-,.-n Cr
ei
0
4
0
Fig. 20. Penetration Curve for Ikon and Chromium i n the Cold Leg (46OOC) of NCL-12 (Croloy 9M), Which Operated f o r 14.40 h r i n Fluoroborate
salt.
systems containing such salts.
The use of loops of an old design pre-
vented our having any removable specimens, but permanent hot-leg specimens
were used i n NCL-12. Our expectation, based on previous experience with fluoride salts,
was t h a t temperature gradient mass transfer of the l e a s t noble constituent (i.e., chromium and iron) would be the limiting factor. But salt analyses after the t e s t indicated t h a t all the major alloying elements of the container materials had mass transferred. The nonselective attack was a l s o confirmed by metallographic examination and microprobe analysis of the loop specimens and piping. I n view of the movement of nickel and molybdenum, it is obvious that highly oxidizing conditions, due t o water and oxygen i n the salt, were present during the operation of the loops.
In analyzing NCL-10 and -12, we reviewed e a r l i e r studies8 ( l a t e 1950's) t o single out the cases of mass transfer of nickel and molybdenum. 8J. H. DeVan, unpublished data, 1957-1959.
z
29
b
We found several instances where t h i s had occurred i n salts containing KF.
c
One such loop, constructed of HastelIoy N, operated for a year with
a NaF-LiF-KF salt (11.5-46.5-42
mole
$1
with a temperature difference of 9OOC. i
a t a max-
temperature of 690°C
No analysis for oxygen or water
was made before t e s t . Examination a f t e r t e s t disclosed green crystals embedded i n the salt. S a l t analyses showed significant increases i n nickel, iron, molybdenum, and chromium content. X-ray analysis showed that the green crystals were mixtures of sodium and potassium chromium fluoride complex compounds and that most of the XI? present i n the salt was actually KF-2H20. Another loop, constructed of Inconel, (~i-18%Cr-lO$
Fe) operated
about one-half year with the same salt and a t the same temperatures as above.
After t e s t , metallographic examination showed heavy attack i n
the hot-leg portion of the loop.
After t e s t only the chromium and iron
contents of the salt were determined; the chromium content had increased significantly from 60 t o 900 ppm. X-ray analysis of the salt disclosed that the salt was about 15%KF-2H20.
The relatively well-defined x-ray
pattern of t h i s hydrate suggested that it was not formed when the cold melt was exposed t o a i r but was carried as a part of the salt mixture during operation.'
The compound KFe2H20 is knuwn t o be thermally stable.
The l i t e r a t u r e s t a t e s that KF easily forms a series of crystal hydrates, whereas LiF and NaF crystallize ar~hydrously.~It is a l s o noted t h a t it
is easy t o form KBF3OH and NaBF3OH and that they are quite stable. Thus we have seen that during the molten-salt reactor corrosion program, salts containi metals.
We believe
ciated with t h a t a l k a l i found no leakage of .
b
have on occaSion been very aggressive toward
is is the coxtibinedwater assofluoride salt. We again s t r e s s that we of the loops.
This suggests t h a t
hydrated KF is not r
purification process.
it appears t h a t con21 released and w i l l reac
the fluoroborate salt mixture can be
Paradoxically, c
-.
*â&#x201A;ŹE' + BF3OH
(2)
'1. G. Ryss, The Chemistry of Fluorine and Its Inorganic Compounds, pp. 521-28 and 815-16, AEC-tr-3927, Pt. 2, (February 1960).
30 The generation of HF i n the system leads t o the following reactions with
the elements of the container material: 2HF
, + 3H2 , + H2 , + H2 .
+ N i eNiF2 +
6HF + b * k F 6 2HF + Fe t F e F 2 2HF + C r t C r F 2
(3 1
H2
(41 ( 51
(6
Note that, i n the temperature range of interest, changes i n the standard free energy of formation are not favorable f o r all the reactions
as written. scheme"
However, studies on the Fluoride Volatility Processing
a t ORNL shawed that i n a Hastelloy N hydrofluorinator containing
fused fluoride salts and HF, chromium and iron were rapidly leached f r o m the alloy at elevated textperatures (500 t o 650째C) even when the HI? activi t y w a s quite law.
The main reaction i s the oxidation of the metal by
the HF t o form fluorides soluble i n the melt.
It was found t h a t NiF2 i s
produced by driving the reaction through the continuous removal of hydrogen and reaction products, since the free energy of formation (above 49OOC) of the nickel fluoride reaction by Eq. (3) is not favorable.
For
the same reason, molybdenum can also be forced t o react with HF even though a positive change i n free energy is involved.
Evidence of s m a l l
but f i n i t e dissolution rates of molybdenum metal during hydrofluorination conditions have been reported.
l2
In l i g h t of the discussion above, we can now consider why two different types of products (i.e.,
metal and fluoride compounds) were mass
transferred i n these (NCL-10 and 1 2 ) thermal convection loops. 11
''A. P. Litman and R. P. Milford, Corrosion Associated with the Oak R i d g e National Laboratory Fused S a l t Fluoride Volatility Process, I t paper presented a t the Symposium on &sed Salt Corrosion a t the Fall
Meeting of the Electrochemical Society, Detroit, Michigan, Oct. 1-5, 1961. "A. E. Goldman and A. P. Litman, Corrosion Associated With Hydrofluorination i n the.Oak Ridge National Laboratory Fluoride Volatility Process, ORNL-2833 (November 1961).
12A. P. Litman, Corrosion of Volatility Pilot mant MARK I INOR-8 Hydrofluorinator and MARK I11 L Nickel Fluorinator After Fourteen Dissolution Runs, ORNL-3253 (Feb. 9, 1962).
z
t
31 Thermodynamics of System Corrosion The cycle of mass transfer i n i t i a t e d by the corrosion of metals by
fluoride salts i s k n m t o begin i n the hotter regions of a loop system w i t h the formation of structural metal fluorides t h a t are soluble i n the
salt : M+F'-==M!?
-,
(7)
'
where M is the attacked metal of the container. The equilibrium constant for Eq. (7) increases with increasing temperature; thus, i n a Multicomponent alloy the concentration of the attacked c o q t i t u e n t , M, w i l l decrease at loop surfaces a t high temperature (weight loss) and increases a t surfaces a t l m e r temperatures (weight gains).
A t some intermediate temperature, the i n i t i a l surface composi-
t i o n of the structural alloy w i l l be i n equilibrium with the fised salt (no weight change).
In the cooler regions of a closed system, the r a t e a t which the metal is deposited (steady s t a t e condition before plugging) i s generally equal t o the r a t e at which it diffuses into the metal maintain i t s equilibrium a c t i v i t y on the surface.
- a necessity t o
Thus the r a t e of
diffusion of the metal i n the alloy i n the cooler regions usually cont r o l s the r a t e of corrosion i n the hot zone.
A t t h i s stage i n the tem-
3
perature-gradient mass-transfer process, weight gains would be found on specimens i n the cold section but l i t t l e i f any surface change (deposits) would be seen. This generalization is valid only when the equilibrium concentration of a metal Eq.
(711
does not exceed
e compound i n the salt [produced by ation concentration of a metal fluoride
compound i n the salt at the l a w temperature. Early studies reported by Grimes13 clearly i l l u s t r a t e these points. Table 6 shms the chromium concentrations for two salts as functions of the equilibrium between the salts and Inconel or pure chromium. t h a t when the alkali-met
Note
fluoride salt (NaF-fCF-LiF-UF4) i s i n contact
with Inconel a t 800째C it w i l l support a higher concentration of chromium 13W. R. Grimes,
pp- 96-99.
ANP &uart. Progr. Rept. June 10, 1956, Om-2106
32 Table 6.
crd
Equilibrium Concentrations of Chromium Fluorides W i t h !bra S a l t s
t
Chromium Concentration (ppm) NaF-KF-LiF-UF4
NaF-ZrF4 -UT4
Calculated salt equilibrium with Inconel
Ncr =
0.16 a t 800째C (ref. a )
1660
1400
1100
2400
Experimental salt equilibrium with pure chromium
Ncr =
1.0 a t 600째C (ref. a > ~~
'concentration of chromium i n mole fraction. fluorides
(1660 ppm Cr) than it w i l l when it is i n contact with pure
chromium a t 600째C (U00 ppm C r ) salt in
.
Accordingly, circulation of such a
an Inconel loop would result i n the deposition of essentially
pure chromium metal i n the cold zone.
In that case, the t o t a l r a t e of
attack would be controlled simply by diffusion of chromium t o the interface between metal and salt in the hot zone.
W e believe that the deposi-
tion of pure iron i n NCL-12 (Croloy 9M) occurred t h i s way.
This i s not
a new phenomenon.
Rapid plugging by deposition of metal dendrites occurred frequently in the l a t e 1950's especially i n iron-base alloy loops. 14, l 5 Examination of the data f o r the other s a l t sham i n Table 6 (NaF-ZrFc-UF4) leads t o the conclusion that chromium metal would not p l a t e out i n t h a t system and t h a t any product of mass transfer would be
a fluoride compound. A t 600째C t h i s salt i n equilibriumwith pure chromium w i l l support a higher concentration of chromium fluorides than it w i l l I 4 G . M. Adamson, R. S. Crouse, and W. D. W y , Interim Report on Corrosion by Alkali-Metal Fluorides: Work t o k y 1, 1953, ORNL-2337 (March 20, 1959). 15G. M. Adamson, R. S. Crouse, and W. D. Manly, Interim Report on Corrosion by Zirconium-Base Fluorides, ORNL-2338 (Jan. 3, 1961).
I
33
i n contact with Inconel at 800째C.
For gross deposition of compounds t o occur, the concentration of the compound a t the temperature of interest (cold zone) must exceed the saturation concentration of the metal fluoride corrosion product present in the system. We believe t h a t the mechanism i n NCL-10 (Hastelloy N) i s similar t o the one discussed above for the NaF-ZrF4 system and t h a t i n time the con-
- or more accurately the concentration of mixed metal chromium fluoride - i n the fluoroborate salt at 605째C exceeded the centration of chroplium
saturation concentration a t 460째C and allowed deposition of large quant i t i e s of complex compounds. Both NCL-10 and NCL-12 operated with the same salt a t the same temperature, yet they were plugged by different mechanisms at different
rates. A chromium-rich plug was found i n the Hastelloy N loop (containing 7$ C r 3 $ Fe) and an iron plug was found i n the Croloy 9M loop (containing 9%C r - b a l Fe). Thus, it appears t h a t when these fluoroborate salts are contained i n a l l o y s w i t h between 7 and 9 w t 4 Cr, the iron content of the alloy controls the composition of the temperature-gradient mass-transfer deposit. i
Kinetics of System Corrosion With the foregoing mine when plugging start element a t various times. We calculated the weight of the iron plug
an assumed reaction-rate constant and mode
i n the cold section, 70
&Ir
oncentrations for chromium and iron i n amount of these elements a f t e r t e s t , the
culations, presented i n T
i
n NCL-10 and -12 and the disposition of each
NCL-12 from knowledge o of chemical attack (from 1
c
and evaluation, it is now possible t o deter-
xperiments). l6
The results of the cal-
, show that
the saturation value of iron 1120 mg, was exceeded shortly after
130 hr; at t h a t time pure started depositing and eventually caused a complete plug. Table 8 shows the same kind of calculations f o r the operation of NCL-10. In t h i s case, it appears t h a t the saturation W u e of chromium 16J. W. Kbger and A. P. Litman, M SR Program Semi-. Feb. 29, 1968, ORNL 4254 pp. 218-225.
Progr. Rept.,
\
Table 7.
Calculated Concentration of Alloying Elements from NCL-12 Present i n the S a l t a t Various Times Concentration i n Salt
Maximy Attack
Time (hr)
(%/an21
14.4 57.6
Average Attack (mg/cm2)
Area Attackedb (an21
Total
Material
Deposited i n Ribbon Form
Lost (mg)
Fe
(w)
Deposited As P l w (mg)
Cr
(mg)
(ppm)
(mg)
(ppm)
2 4
1 2
650 650
650 1300
250 500
360 720
225 450
40 80
25 50
130
6
3
650
1950
750
1080
675
120
75
1440
20
10
650
6500
2450
1120
700'
400
250'
'Calculated
from LW = 2/&
where K = rate constant,
p
& an2/sec a t 6070C,
LW = weight loss, c = concentration of chromium and iron, P = density
of Croloy 9M, and
t = time. bIncludes surge tank and l i n e s and one-half of t o t a l area. C
By chemical analysis.
.
2530
:
Table 8.
Calculated Conceritration of Alloying Elements from NCL-10 Present in the Salt at Various Times Concentration
Th? 4000 8760
Mt-l&m Attack& brig/cm* ) 38: 56
Average Area Attack Attackedb blg/u!l* > ,h?m2) 19 28
550 556
Deposited on TotE!l Material Cold Surface "l.ost bug> 10,450 15,400
2100 3300
in Salt Deposited
Cr
Fe
Ni
MJ Arlmgp;ukl
h3)
(ppm)
brig)
(ppm)
bg)
Cppm)
bug)
350 509
383 555c
420 427
459 470'
6350 9300
6950 ll50 10,OOOc 1560
(ppm) 1260 1700'
220 %
aCsbul.ated f&m &I = 2/J p & where K= rate constant, 10-l* cm*/sec at 607Y, LS?= weight loss, c = concentration of chromium, iron, nickel, and molybdenum, P = density of Hastelloy N, and ,. t .= time. b Includes surge tank and lines and one-half' total area.
36
i n the cold leg, 470 ppm, was reached a f t e r about 4000 h r of operation;
W
a t that time, the chromium, as Na3CrF6, started depositing i n large amounts. 17
Y
It i s interesting t o note t h a t i n both cases the amounts of the alloying elements i n the salt and i n the plug were i n about the same r a t i o as they are i n the base metal.
Capsule t e s t s and other loop t e s t s
have shuwn t h a t when constituents of an alloy react w i t h the l i q u i d medium they w i l l be found i n the liquid and/or deposited i n the r a t i o at which they existed i n the alloy. l8 This behavior was found i n both loops of t h i s experiment. Nickel and molybdenum mass transfer products, not normally found i n relatively pure fluoride salt systems, also follow t h i s pattern.
As has
been stressed here, the presence of gross quantities of nickel and molybdenum indicates strongly oxidizing conditions. Salt Purification
The salt used i n these experiments contained many impurities that the old techniques, successful with other fluoride salts, did not remove. Since these experiments, improvements have been made i n the fluoroborate
salt preparation. Only very pure salt (99.9%) is now used as s t a r t i n g material. I n fact, the salt has so few impurities t h a t no steps are "Several suggestions, besides the removal of the water or oxygen from the system, are offered t o improve the service of the container materials using t h i s fluoroborate salt. The most obvious change is t o lower the hot-leg temperature t o 540째C thus lowering the reaction-rate constant an order of magnitude. It would then take three times as long t o duplicate the previous plugging. Another possibility is t o r a i s e the temperature i n the cold-leg section. This would r a i s e the saturation value of the elements i n the salt, and depositing would not occur u n t i l later. But t h i s probablywould not improve the l i f e by the same factor as above. Probably the most important improvement i s removing corrosion broducts from the system on a continuous or batch-wise basis since deterioration (thinning) of the container w a l l by dissolutive corrosion i s not a probled i n these systems. 18J. R. Weeks and D. H. G u r i n s Q , "Solid MeW-Liquid Metal Reactions i n Bismuth and Sodium," pp. 106-161 i n L i q u i d Metals and Solidification, American Society for Metals, Metals Park, Novelty, Ohio, 1958.
P
-
37 taken during processing t o remove the structural metals.
Purification procedures f o r removing water and oxygen are now under study. A new procedure is also used i n the melting and preparation of the fluoroborate
salt t o prevent loss of BF3 vapor and the ensuing change of composition. f
In brief, the loaded salt i s evacuated t o about 380 t o r r and heated t o 150째C i n a vessel lined w i t h nickel .and i s held for about 15 h r under these conditions.
If the r i s e i n vapor pressure i s not excessive, (no
v o l a t i l e impurities) the salt i s heated t o 5OO0C, while s t i l l under vacuum, and agitated w i t h helium for a few hours.
The salt i s then
ready for transfer t o the f i l l vessel. CONCLUSIONS
1. Natural circulation loops, fabricated from Hastelloy N and
Croloy 9% t h a t circulated impure (> 3000 ppm impurities) NaBF4-NaF-KBF4 (90-4-6 mole
4)
a t a maximum temperature of 605째C with a temperature
difference of 145째C evidenced serious temperature-gradient mass transfer. The mass transfer involved migration of all major constituents of the constituents of the container materials and resulted i n r e s t r i c t i n g f l o w i n i
the Hastelloy Nloop by deposition of Na3CrF6 crystals and complete plugging of the Croloy 9M loop by iron dendrites. 2.
The nonselective corrosion observedwas due t o the presence
of water, chemically bound t o the fluoroborate salts, that reacted during heating t o form HI?. 3.
The driving force
mass transfer was the temperature depen-
dence of the equilibrium constant between the container material cons t i t u e n t s and the most stable fluoride compounds that can form i n the
system. 4.
The saturation concentrations for iron and chromium i n the t e s t
salt a t 460째C were found t o be 700 and 470 ppm, respectively. C
i
b'
1. Other, more highly purified fluoroborates should be extensively
tested f o r corrosion before these coolants can be qualified for moltensalt reactor service.
38 2.
Based on knowledge t o data, iron-base and iron-containing alloys
w
should be avoided i n molten-salt reactor coolant circuits t h a t use fluoroborate salts.
ACKNCWLEDGMEXTS
t
It i s a pleasure t o acknowledge t h a t E. J. Lawrence supervised con-
struction, operation, and disassenibly of the t e s t loops during the course
of t h i s program. We are also indebted t o H. E. McCoy, Jr. and J. H. DeVan for constructive review of the manuscript. Special thanks are extended t o the Metallography Grow, especially H. R. Gaddis, H. V. Mateer, and R. S. Crouse, and t o the Analytical
Chemistry Division, Graphic Arts Department, and the Metals and Ceramics Division Reports Office f o r invaluable assistance.
i
39 Om-TM-2490
INTERNAL DISTRIBUTION 1-3. 4-5.
Central Research Library ORNL Y-12 Technical Library Document Reference Section 6-15. Laboratory Records 16. Laboratory Records, ORNL RC 17. ORNL Patent Office 18. R. K. Ad19. G. M. Adamson 20. R. G. Affel 21. J. L. .Anderson 22. R. F. Apple 23. C. F. Baes 24. J. M. Baker 25. S. J. Ball 26. C. E. m e r g e r 27. C. J. Barton 28. H. F. Batman 29. S. E. B e a l l 30. R. L. Beatty 31. M. J. B e l l 32. N. Bender 33. C. E. Bettis 34. E. S. Bettis 35. D. S. Billington 36. R. E. Blanc0 37. F. F. Blankenship 38. J. 0. Blomeke 39. R. Blumberg 40. E. G. Bohlmann 41. C. J. Borkowski 4 2 . G. E. Boyd 43. J. Braunstein 44. M. A. Bredig 45 R. B. Briggs 46. H. R. Bronste 47. G. D. m t o n 48. D. A. Canonico 49. S. Cantor 50. W. L. Carter . 5 1 G. I. Cathers 52. 0. B. Cavin 53. J. M. Chandler ' 54. F. H. Clark 55. W. R e CObb 56. H. D. Cochran 57. C. W. Collins
-
I
-
58. 59. 60. 61. 62. 63. 64. 65. 66. 67. 68. 69. 70. 71. 72. 73.
74. 75. 76. 77.
78. 79. 80. 81. 82. 83. 84. 85. 86. 87.
88. 89. 90. 91. 92. 93. 94. 95. 96. 97. 98. 99. 100. 101.
102. 103.
E. L. Compere K. v. cook W. H. Cook L. T. Corbin B. Cox R. S. Crouse J. L. Crawley F. L. Culler D. R. Cuneo J. E. Cunningham J. M. Dale D. G. Davis R. J. DeBakker J. H. DeVan S. J. Ditto A. S . Dworkin I. T. Dudley D. A. Dyslin W. P. Eatherly J. R. Engel E. P. Epler D. E. Ferguson L. M. Ferris B. Fleischer A. P. Fraas H. A. Friedman J. H Rye, Jr. W. K. Furlong C. H. Gabbard R. R. Gaddis R. B. Gallaher R. E. Gehlbach J. H. Gibbons L. 0. Gilpatrick P. A. Gnadt R. J. Gray W. R. Grimes A. G. Grindell R. W. Gunkel R. H. Guymon J. P. Hammond B. A. Hannaford P. H. Harley D. G. Harman w. 0. Harms C. S. Harrill
40 1
104. 105. 106. 107. 108. 109-m . 112. ll3.
114. ll5. ll6. ll7.
P. R. P. D. J. M. H. D. P. R. A.
T.
118. W. 119. 120. 121. 122. 123. 124. 125. 126. 127.
H. W. P. R. M. M. C.
T. H.
128. J. 129. D. 130. S.
131-140. 141.
J. R. 142. A. 143. T. 144. J. 145. C. 146. J. 147. C. 148. E. 149. J. 150. M. 151. R. 152-161. A. 162. G. 163. E. 164. A. 165. M. 166. R. 167. R. 168. H. 169. R. 170. J. 171. D. 172 C.
173. W. 174. H.
kubenreich Helms Herndon Hess Hightawer Hill HofHolmes Holz Horton Houtzeel L. Hudson R. Huntley Inouye H. Jordan R. &sten J. Kedl T. Kelley J. Kelley R. Kennedy W. Kerlin T. Kerr J. Keyes V. Kiplinger S. Kirslis W. Koger B. K o r s m e y e r I. Krako-dak S. Kress W. Krewson E. Lanib A. Lane E. Larson J. Lawrence J. Lawrence S. Lin B. Lindauer P. Litman H. Llewellyn L. Long, Jr. L. Lotts I. Lundin N. Lyon L. Macklin G. MacPherson E. IkcPherson C. M a i l e n L. Ma,nning D. Ma,rtin R. Martin V. Mateer N. E. G. N. R. R. W. K. P. W.
T. H. R. 178. H. 179. D. 180. C. 181. C. 182. L. 183. J. 184. H. 185. A. 186. R. 187. R. 188. D. 189. T. 190. K. 191. H. 192. J. 193. E. 194. E. 195. L.
175. 176. 177
196.
197. 198. 199. 200 201. 202. 203. 204. 205. 206. 207. 208. 209. 210. 2ll. 212. 213. 214. 215. 216. 217. 218. 219. 220. 221. 222. 223. 224. 225.
P. A. T. H. B. G. J. M. G. R. W. K. R. H. W. C.
H. Mauney McClain W. McClung E. McCoy L. McElroy K. McGlotNan J. McHargue E. McNeese R. M c W h e r t e r J. Metz S. E y e r P. Milford L. Moore M. Moulton W. Mueller A. N e l m s H. N i c h o l P. N i c h o l s L. N i c h o l s o n D. N o g u e i r a C. W e s Patriarca M. Perry W. Pickel B. Piper E. Prince
ic,
*
L. Ragan
L. R e d f o r d Richardson D. R o b b i n s C. R o b e r t s o n C. R o b i n s o n A. R o n i b e r g e r G. R o s s C. Savage F. Schaffer E. S c h i l l i n g Dunlap Scott J. L. Scott H. E. Seagren C. E. Sessions J. H. Shaffer W. H. Sides G. M. Slaughter A. N. Smith F. J. Smith G. P. Smith 0. L. Smith P. G. Smith I. Spiewak R. C. Steff'y
t
fc
W
41
ld Y
3
226. 227. 228. 229. 230. 231. 232. 233 234. 235. 236. 237. 238. 239. 240.
.
W. C. Stoddart H. H. Stone R. A. Strehlm D. A. Sundberg J. R. Tallackson E. H. Taylor W. Terry R. E. Thoma P. F. Thomason L. M. Toth D. B. Trauger W. E. Unger G. M. Watson J. S. Watson H. L. Watts
241. 242. 243 244. 245. 246. 247. 248. 249. 250. 251. 252. 253. 254. 255.
.
F. Weaver H. Webster M. Weinberg R. Weir J. Werner K. W. West M. E. Whatley J. C. White R. P. Wichner L. V. Wilson Gale Young H. C. Young J. P. Young E. L. Youngblood F. C. Zapp
C. B. A. J. W.
EXTERNAL DISTRIBUTION
0
4
256. 257. 258. 259. 260. 261. 262. 263. 264. , 265. 266-267. 268. 269. 270. 271. 272. 273. 274. 275. 276. 277. 278. 279. 280. 281. 282. 283. 284+98.
G. J. D. C. H.
G. Allaria, Atomics International G. Asquith, Atomics International F. Cope, RDT, SSR, AEC, Oak Ridge National Laboratory B. Deering, AEC, OSR, Oak Ridge National Laboratory M. Dieckamp, Atomics International A. Giauibusso, AEC, Washington F. D. Haines, AEC, Washington C. E. Johnson, AEC, Washington W. L. Kitterman, AEC, Washington W. J. Larkin, AEC, Oak Ridge Operations T. W. McIntosh, AEC, Washington A. B. Martin, Atomics International D. G. Mason, Atomics International C. L. Matthews, RDT, OSR, AEC, Oak Ridge National Laboratory G. W. eyers, Atomics International D. E. Reardon, AEC, Canoga Park Area Office H. M. Roth, AEC, Oak Ridge Operations M. Shm, AEC, Washington J. M. Simmons, AEC, Washington W. L. SmaUey, AEC, Washington S. R. Stamp, AEC, Canoga Park Area Office E. E. Stansburg, the University of Tennessee D. K. Stevens, AEC, Washington R. F. Sweek, AEC, Washington A. Taboada,- AEC, Washington R. F. Wilson, Atomics International Laboratory and University Division, AEC, Oak Ridge Operations Division of T nformation Extension