Knowledge

External Active Thermal Control System

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160: 148: 234: 196: 128:, and various sensors for monitoring performance. The Nitrogen Tank Assembly (NTA) controls the flow of ammonia out of the Ammonia Tank Assembly (ATA). The ATA contains two flexible, chambers incorporated into its ammonia tanks that expand as pressurized nitrogen from the NTA expels liquid ammonia out of the ATA. The major components in the ATA include two ammonia storage tanks, isolation valves, heaters, and various temperature, pressure, and quantity sensors; 222: 36: 28: 137: 172: 246: 184: 208: 258: 20: 131:
Heat Rejection - Ammonia passes from the ATA through a two way path of the Flex Hose Rotary Coupler (FHRC) where heat captured while passing through the Heat Exchangers is directed to be expelled through the Heat Rejection System Radiators (HRSRs). The radiators are rotated by the Thermal Rotary
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Heat Transportation - The Pump Module (PM) provides flow and accumulator functions and maintains proper temperature control at the pump outlet for each Loop. The PM consists of a single pump, a fixed charge accumulator, a Pump & Control Valve Package (PCVP) containing a firmware controller,
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in closed-loop circuits. The EATCS is capable of rejecting up to 70 kW, and provides a substantial upgrade in heat rejection capacity from the 14 kW capability of the Early External Active Thermal Control System (EEATCS) via the Early Ammonia Servicer (EAS), which was launched on
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as well as cold plates under three DC-to-DC Conversion Units (DDCUs) (one DDCU each on each Loop on the P1/S1 Trusses and two DDCUs each on each Loop on the S0 Truss) and two Main Bus Switching Units (MBSUs) on each Loop on the S0 Truss (see schematic below and
269: 51:(EATCS) maintains an equilibrium when the ISS environment or heat loads exceed the capabilities of the Passive Thermal Control System (PTCS). Note Elements of the PTCS are external surface materials, insulation such as 387: 343: 348: 233: 159: 99:
There are two independent Loops (Loop A & Loop B) that combined make up the EATCS. The EATCS Loops perform three primary functions:
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Trusses. The EATCS consists of two independent Loops (Loop A & Loop B), which both use mechanically pumped fluid state
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Radiator Joint (TRRJ) which continually rotates the radiator wing for optimum cooling.
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Heat Collection - Each Loop draws heat from five Heat Exchangers (HXs) mounted on the
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ISS External Active Thermal Control System (EATCS) diagram
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capabilities for all the U.S. pressurized modules, the
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Electrical system of the International Space Station
296: 294: 16:International Space Station thermal control system 302:"Active Thermal Control System (ATCS) Overview" 239:FHRC without MLI cover and in situ on the TRRJ 388:Components of the International Space Station 349:Environmental Control and Life Support System 8: 18: 290: 217: 143: 49:External Active Thermal Control System 272:EATCS components on the S1/P1 Trusses 251:Heat Rejection System Radiator (HRSR) 7: 120:(ORUs) for design of these units); 14: 256: 244: 232: 220: 206: 194: 182: 170: 158: 146: 227:Flex Hose Rotary Coupler (FHRC) 373:Scientific research on the ISS 1: 177:Nitrogen Tank Assembly (NTA) 326:International Space Station 213:ATA drawing (cover removed) 201:Ammonia Tank Assembly (ATA) 189:NTA drawing (cover removed) 45:International Space Station 404: 332:Integrated Truss Structure 65:Japanese Experiment Module 367:ExPRESS Logistics Carrier 361:External Stowage Platform 338:Orbital Replacement Units 118:Orbital Replacement Units 69:Columbus Orbital Facility 355:Integrated Cargo Carrier 140:EATCS schematic overview 92:and installed onto the 281: 273: 141: 53:Multi-Layer Insulation 40: 39:DDCU cold plate design 32: 31:Early Ammonia Servicer 24: 280:TCS System of the ISS 279: 271: 139: 59:. The EATCS provides 38: 30: 22: 282: 274: 142: 105:Destiny Laboratory 41: 33: 25: 124:startup heaters, 395: 313: 312: 306: 298: 260: 248: 236: 224: 210: 198: 186: 174: 162: 153:Pump Module (PM) 150: 126:isolation valves 403: 402: 398: 397: 396: 394: 393: 392: 378: 377: 322: 317: 316: 304: 300: 299: 292: 287: 264: 261: 252: 249: 240: 237: 228: 225: 214: 211: 202: 199: 190: 187: 178: 175: 166: 163: 154: 151: 17: 12: 11: 5: 401: 399: 391: 390: 380: 379: 376: 375: 370: 364: 358: 352: 346: 341: 335: 329: 321: 318: 315: 314: 289: 288: 286: 283: 266: 265: 262: 255: 253: 250: 243: 241: 238: 231: 229: 226: 219: 216: 215: 212: 205: 203: 200: 193: 191: 188: 181: 179: 176: 169: 167: 164: 157: 155: 152: 145: 134: 133: 129: 121: 61:heat rejection 15: 13: 10: 9: 6: 4: 3: 2: 400: 389: 386: 385: 383: 374: 371: 368: 365: 362: 359: 356: 353: 350: 347: 345: 342: 339: 336: 333: 330: 327: 324: 323: 319: 310: 303: 297: 295: 291: 284: 278: 270: 259: 254: 247: 242: 235: 230: 223: 218: 209: 204: 197: 192: 185: 180: 173: 168: 161: 156: 149: 144: 138: 130: 127: 122: 119: 114: 110: 106: 102: 101: 100: 97: 95: 91: 86: 82: 78: 74: 70: 66: 62: 58: 54: 50: 46: 37: 29: 21: 308: 263:HRSR drawing 98: 48: 42: 67:(JEM), the 285:References 165:PM drawing 57:Heat Pipes 55:(MLI), or 382:Category 320:See also 351:(ECLSS) 96:Truss. 90:STS-105 85:ammonia 369:(ELCs) 363:(ESPs) 357:(ICCs) 340:(ORUs) 113:Node-3 111:& 109:Node-2 47:(ISS) 334:(ITS) 328:(ISS) 305:(PDF) 309:NASA 79:and 43:The 384:: 307:. 293:^ 107:, 94:P6 81:P1 77:S1 75:, 73:S0 311:.

Index




International Space Station
Multi-Layer Insulation
Heat Pipes
heat rejection
Japanese Experiment Module
Columbus Orbital Facility
S0
S1
P1
ammonia
STS-105
P6
Destiny Laboratory
Node-2
Node-3
Orbital Replacement Units
isolation valves

Pump Module (PM)
PM drawing
Nitrogen Tank Assembly (NTA)
NTA drawing (cover removed)
Ammonia Tank Assembly (ATA)
ATA drawing (cover removed)
Flex Hose Rotary Coupler (FHRC)
FHRC without MLI cover and in situ on the TRRJ
Heat Rejection System Radiator (HRSR)

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