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ANP PROlECT PROGRESS REPORT - t - W I 350 /< // 5 y 300 I / '/ '0 / 250 ' 0' a a 'I/ 200 . A 0- 5 4 I A 150 ,-A I I 100 50 I I *A- I I I I? 0 et ORNL mcm% I-DWG 14955 0 200 400 600 800 4000 t 200 1400 1600 1800 2000 FLOW (gprn) Fig. 1.4.3. ART Primary NaK Pump (Model PK-P) Performance Curves of Head vs Flow Showing - - - Efficiency and Volute Pressure Balance Lines. 0.030 in. and the optimum radial clearance to be 0.015 in. These clearances will result in a bypass flow rate of 3 to 6 gpm at 1220-gpm pump-discharge flow. Static deflection tests were made on the pump shaft used in the water test rig and on the lnconel pump shaft to be used in the final pumps. The information obtained, along with the calculated deflection of the lnconel pump shaft during high- temperature operation, indicated that a top labyrinth 52 seal radial clearance of 0.015 in. should be sufficient to prevent rubbing of the impeller hub against the top labyrinth seal. These water tests of the primary NaK pump indi- cate that the pump will meet the head and flow conditions required for the ART. A pump tank gas pressure of 10 psigshould be sufficient to suppress cavitation at the design flow rate and up to a NaK temperature of approximately 138OOF. The design conditions are in the range of minimum volute ,- hydraulic unbalance. LiJ
c' I - + r 500 450 400 3 50 300 2 250 W I 200 I50 100 50 - - - HEAD I 1 h -- ---. - ORNL-LR-DWG 14956 200 0 0 200 300 400 500 600 700 800 900 to00 1100 I200 1300 1400 1500 I600 1700 FLOW (gpm) Fig. 1.4.4. ART Primary NaK Pump (Model PK-P) Performance Curves Showing Shaft Horsepower vs Flow. 180 I60 I 140 ' s LL LT W c4 120 3 z 0 n W v) 100 5 a W 80 2 a 0 I I- 60 $ 40 20 v)
Page 3 and 4: Part 1 AIRCRAFT REACTOR ENGINEERING
Page 5 and 6: STATUS OF ART DESIGN Design work on
Page 7 and 8: of pressure loads. The idealized mo
Page 9 and 10: UPPER DECK 7 @ PRESSURE SHEL PERIOD
Page 11 and 12: SOD,UM r--- INCONEL TANK ROOF 0 0.5
Page 13 and 14: TABLE 1.1.1. NaK PUMP SPEEDS AND HO
Page 15 and 16: 62 CALCULATED HEATING (w/crn3) N w
Page 17 and 18: where I = radius of source (taken a
Page 19 and 20: heat exchanger was used. The heatin
Page 21 and 22: head which are bounded by various t
Page 23 and 24: h bd * W - EcBRc+ ORNL-LR-DWG I4918
Page 25 and 26: PERIOD ENDlNC JUNE 10. 1956 TABLE 1
Page 27 and 28: ENRICHER ACTUATOR J. M. Eastman Spe
Page 29 and 30: hd - Thus, even with an input signa
Page 31 and 32: - . 140 120 p 100 g d 80 8 L s In y
Page 33 and 34: and lose their hardness in the pres
Page 35 and 36: p. W 2.5 0.5 0 400 OPERATING TIME (
Page 37: i 20 too 80 40 20 PERIOD ENDING JUN
Page 41 and 42: 01) 0V3H 5: N 0 2 s 0 0 0 5: 0 2 s
Page 43 and 44: the first 200OF and B0F/sec for the
Page 45 and 46: PERIOD ENDING JUNE 10, 1956 TABLE 1
Page 47 and 48: L 0 _, I, -* t; - PERIOD ENDING JUN
Page 49 and 50: LJ 0.005 in. on the diameter and a
Page 51 and 52: I 3 -I W CALROD HEATER 1500 I 1400
Page 53 and 54: -17 Inconel I .._I_ I" .. _ _ ~ ._
Page 55 and 56: i E ART FACILITY F. R. McQuilkin Co
Page 57 and 58: L7i PERIOD ENDING JUNE 10, 1956 Fig
Page 59 and 60: PERIOD ENDING JUNE 10, 1956 Fig. 1.
Page 61 and 62: ART OPERATING MANUAL W. B. Cottrell
Page 63 and 64: Part 2 CHEMISTRY W. R. Grimes
Page 65 and 66: W 2.1. PHASE EQUILIBRIUM STUDIES' C
Page 67 and 68: - 0 Q 3 G 4000 900 800 700 a w a 5
Page 69 and 70: - a t a w 1000 900 000 - P 700 3 2
Page 71 and 72: - 0 e 4 000 900 800 5 700 I- a a W
Page 73 and 74: ZrF4 9t2 PERIOD ENDING JUNE 10, 795
Page 75 and 76: U c * NaF*BeF2-2NaF*BeF2 triangle c
Page 77 and 78: THE SYSTEM MgF2-CaF2 L. M. Bratcher
Page 79 and 80: 2.2. CHEMICAL REACTIONS IN MOLTEN S
Page 81 and 82: I id PERIOD ENDING JUNE 10, 1956 an
Page 83 and 84: PERIOD ENDlNG JUNE 10, 1956 V which
Page 85 and 86: u the salt-metal interface, and the
Page 87 and 88: of this reaction will be made at th
Page 89 and 90:
+- + z 6 e 6 5 3 3 > k i m 3 2 2 1
Page 91 and 92:
FeF,. The FeF, saturation points we
Page 93 and 94:
UNIF, = yN should be unity (a pure
Page 95 and 96:
Although it appears that the solubi
Page 97 and 98:
, . 2.3. PHYSICAL PROPERTIES OF MOL
Page 99 and 100:
-0 a rn u) u) DO2 oot c ;o rn OS g
Page 101 and 102:
IL, - PERIOD ENDING JUNE 70, 7956 O
Page 103 and 104:
8 00 700 600 - 0 0, w 500 a 3 I- U
Page 105 and 106:
supporting plaque is loaded into th
Page 107 and 108:
u 2.4. PRODUCTION OF FUELS c G. J.
Page 109 and 110:
half of fiscal year 1957. This esti
Page 111 and 112:
2.5. COMPATIBILITY OF MATERIALS AT
Page 113 and 114:
volume of 1 M tartaric acid solutio
Page 115 and 116:
After the trap has been opened, bot
Page 117 and 118:
\ Part 3 METALLURGY W. D. Manly
Page 119 and 120:
FLUORIDE FUEL MIXTURES IN INCONEL F
Page 121 and 122:
PERIOD ENDING JUNE 10, 1956 TABLE 3
Page 123 and 124:
Fig.3.1.3. Region of Maximum Attack
Page 125 and 126:
(d . terminated after 1217 and 1339
Page 127 and 128:
- . LJ BRAZING ALLOYS IN LIQUID MET
Page 129 and 130:
PERIOD ENDING JUNE 10, 1956 NaK wer
Page 131 and 132:
I PERIOD ENDING JUNE 10, 1956 I Fig
Page 133 and 134:
0. PERIOD ENDING JUNE 10, 1956 Fig.
Page 135 and 136:
Fig. 3.2.10. Apparatus for Studying
Page 137 and 138:
STATIC TESTS OF INCONEL CASTINGS R.
Page 139 and 140:
t (JnOOSll 3n918-3NOt IOH (JoOOSI)
Page 141 and 142:
after the l00hr test. The extent of
Page 143 and 144:
tests of the Lindsay Mix specimens,
Page 145 and 146:
LJ DEVELOPMENT OF NICKEL-MOLYBDENUM
Page 147 and 148:
LJ PERIOD ENDING JUNE 10, 1956 Fig.
Page 149 and 150:
2. Canning of the billets with '/,-
Page 151 and 152:
165 . c, e . c3 a PERIOD ENDING JUN
Page 153 and 154:
u allow the billet to start through
Page 155 and 156:
NEUTRON SHIELD MATERIAL FOR HIGH-TE
Page 157 and 158:
PERIOD ENDfNG JUNE 10, 7956 Fig. 3.
Page 159 and 160:
wrought plate used as base material
Page 161 and 162:
J point. A mixture of 50-50 vol % L
Page 163 and 164:
WELDING PROCEDURE: VERTICAL FIXED,
Page 165 and 166:
4 2 t 4 2 in. t 2 WCLASSFKO ORNL-LR
Page 167 and 168:
FABRICATION OF JOINTS BETWEEN PUMP
Page 169 and 170:
* h WELDING PROCEDURE PERlOD ENDING
Page 171 and 172:
1 1 6 in. PUMP BARREL t SECTION AA
Page 173 and 174:
'4 x 6 x 20-in. INCONEL PLATES (/*-
Page 175 and 176:
UNCLASSIFIED PHOTO 17248 Fig. 3.4.1
Page 177 and 178:
through the radiator by passing col
Page 179 and 180:
L, . 1 Q t V ERIOD ENDING JUNE 10,
Page 181 and 182:
to permit the examination of indivi
Page 183 and 184:
LJ . t L t * I LJ Fig. 3.4.33. Tube
Page 185 and 186:
Fig. 3.4.37. Inner Surface of Tube
Page 187 and 188:
EFFECTOF ENVIRONMENTONCREEP- RUPTUR
Page 189 and 190:
PERIOD ENDING JUNE 10, 1956 UNCLASS
Page 191 and 192:
Fig. 35.7. Surface Effect on the St
Page 193 and 194:
44,000 42,000 40,000 - ._ (D 8000 v
Page 195 and 196:
\:r 1 U UNCL 1158 W ioo,ooo 80,000
Page 197 and 198:
fuel mixture (No. 30) NaF-ZrF -UF,
Page 199 and 200:
i u * ‘*$ , .\. The Lindsay Chemi
Page 201 and 202:
6, * c L . c e 4 gi depths greater
Page 203 and 204:
i 4 Part 4 HEAT TRANSFER AND PHYSIC
Page 205 and 206:
4.1. HEAT TRANSFER AND PHYSICAL PRO
Page 207 and 208:
This relationship gives the ratio o
Page 209 and 210:
The parameters of the’experiment
Page 211 and 212:
t Fig. 4.1.7. Fuel Annulus of the V
Page 213 and 214:
uncooled wall temperature that woul
Page 215 and 216:
SHIELD MOCKUP REACTOR STUDY L. C. P
Page 217 and 218:
Liquid (688 to 8986C) I . HT - H3Q
Page 219 and 220:
THERMAL CONDUCTIVITY W. D. Powers T
Page 221 and 222:
cd Fig.4.2.4. Slingers from MTR In-
Page 223 and 224:
a plug when they came in contact wi
Page 225 and 226:
couples were used on this loop to e
Page 227 and 228:
0 20 40 60 80 lo0 I20 440 (60 180 2
Page 229 and 230:
"fast" neutron in a graphite reacto
Page 231 and 232:
eached thermal equilibrium in an in
Page 233 and 234:
0.5 0.4 - a3 l- W z 0.2 0.1 UNCLASS
Page 235 and 236:
TABLE 4.2.3. RESULTS OF EXAMINATION
Page 237 and 238:
U could be evacuated was used for t
Page 239 and 240:
! j * . x - iu I PERlOD ENDlNG JUNE
Page 241 and 242:
CRITICAL EXPERIMENTS FOR THE COMPAC
Page 243 and 244:
. I) a W PERIOD ENDING JUNE 10, 195
Page 245 and 246:
U I I R i c . --. in. long, 18’4,
Page 247:
I, . R t 3 4 . C 7 6 5 W 5 a c3 E4
Page 250 and 251:
1 a
Page 252 and 253:
ANP PROJECT PROGRESS REPORT ot(E) =
Page 254 and 255:
ANP PROJECT PROGRESS REPORT TABLE 5
Page 256 and 257:
ANP PROJECT PROGRESS REPORT TABLE 5
Page 258 and 259:
6 ANP PROJECT PROGRESS REPORT 2 lo7
Page 260 and 261:
ANP PROJECT PROGRESS REPORT GAMMA-R
Page 262 and 263:
ANP PROJECT PROGRESS REPORT 5.3.3,
Page 264 and 265:
ANP PROJECT PROGRESS REPORT A I P I
Page 266 and 267:
ANP PROJECT PROGRESS REPORT SECTION
Page 268 and 269:
ANP PROJECT PROGRESS REPORT .. .._
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