Knowledge

Satélite Tecnológico

Source 📝

758: 489: 767: 635: 81: 40: 809: 777: 979: 1005: 865: 861: 851: 801: 733: 1046: 772: 748: 707: 654: 649: 1084: 1064: 1041: 970: 880: 605: 1024: 1020: 793: 785: 614: 610: 1100:
are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
559: 482: 276: 389: 1095:
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
475: 368:
launch vehicle on 23 August 2003 in an explosion three days before the launch date. This event came to be known as
1122: 1117: 145: 553: 47: 870: 896: 315: 309: 179: 123: 696: 529: 186: 8: 825: 514: 503: 499: 216: 1000: 467: 361: 287:
The primary objective of SATEC was to test the technological equipment embedded in the
900: 236: 789: 402: 260: 169: 461: 426: 753: 743: 299: 268: 226: 1111: 1079: 958: 875: 584: 918: 830: 723: 702: 589: 1059: 1055: 1051: 964: 846: 665: 659: 952: 946: 1014: 1010: 942: 369: 271:
of scientific applications, designed, developed, built and tested by
984: 922: 909: 856: 797: 727: 692: 645: 549: 294:
The SATEC scientific satellite had the following characteristics:
1069: 975: 926: 913: 762: 640: 619: 564: 544: 538: 453: 1074: 905: 805: 781: 687: 568: 534: 272: 360:
SATEC, which had an estimated life of 6 months, was lost with
738: 671: 365: 288: 206: 196: 134: 29: 345: 497: 291:, providing more information for future applications. 392:. Encyclopedia Astronautica. Retrieved 31 March 2017. 332:
The instrumentation shipped in SATEC was as follows:
275:technicians, engineers and scientists working at 1109: 336:Solar generator: Silicon cells generating 20 W 483: 348:receiver: adapted to the conditions of flight 490: 476: 302:with 61 cm x 66 cm x 66 cm 279:(National Institute for Space Research). 351:Transmitter: S-band with BPSK modulation 1110: 471: 13: 342:PCU: with linear series technology 314:Stabilization: By rotation at 120 14: 1134: 447: 305:Mass: 65 kilograms (143 lb) 419: 395: 382: 91:65.0 kilograms (143.3 lb) 1: 375: 259:("Technologic Satellite" in 211:750 kilometres (470 mi) 201:750 kilometres (470 mi) 122:August 23, 2003, 16:30 UTC ( 7: 282: 10: 1139: 355: 327: 1093: 1034: 993: 935: 889: 839: 818: 716: 680: 628: 598: 577: 522: 339:Battery: Type NiCd – 5 Ah 249: 245: 235: 225: 215: 205: 195: 185: 175: 165: 160: 156: 152: 141: 130: 108: 103: 99: 95: 87: 77: 72: 68: 64: 56: 46: 36: 25: 21: 364:in the explosion of the 323:Altitude: 750 kilometers 370:Accident of Alcantara 166:Reference system 73:Spacecraft properties 1123:Satellites of Brazil 759:Optus and Defence C1 506:Orbital launches in 257:Satélite Tecnológico 1118:2003 in spaceflight 464:Gunter's Space Page 320:Precision: 1 degree 18: 431:space.skyrocket.de 407:space.skyrocket.de 161:Orbital parameters 124:Alcântara accident 60:6 months (planned) 16: 1105: 1104: 253: 252: 1130: 511: 510: 509: 492: 485: 478: 469: 468: 458: 441: 440: 438: 437: 423: 417: 416: 414: 413: 399: 393: 386: 310:Heliosynchronous 197:Perigee altitude 180:Heliosynchronous 119: 117: 104:Start of mission 57:Mission duration 19: 15: 1138: 1137: 1133: 1132: 1131: 1129: 1128: 1127: 1108: 1107: 1106: 1101: 1096: 1089: 1030: 989: 931: 885: 835: 814: 768:Molniya-3 No.53 712: 676: 636:Molniya-1 No.92 624: 594: 573: 518: 517: 507: 505: 504: 502: 496: 457:(in Portuguese) 456: 450: 445: 444: 435: 433: 425: 424: 420: 411: 409: 401: 400: 396: 387: 383: 378: 358: 330: 285: 207:Apogee altitude 121: 115: 113: 112:August 25, 2003 12: 11: 5: 1136: 1126: 1125: 1120: 1103: 1102: 1098:Crewed flights 1094: 1091: 1090: 1088: 1087: 1082: 1077: 1072: 1067: 1062: 1049: 1044: 1038: 1036: 1032: 1031: 1029: 1028: 1017: 1008: 1003: 997: 995: 991: 990: 988: 987: 982: 973: 968: 961: 956: 949: 939: 937: 933: 932: 930: 929: 916: 903: 893: 891: 887: 886: 884: 883: 878: 873: 868: 859: 854: 849: 843: 841: 837: 836: 834: 833: 828: 822: 820: 816: 815: 813: 812: 775: 770: 765: 756: 751: 746: 744:Progress M1-10 741: 736: 731: 720: 718: 714: 713: 711: 710: 705: 700: 690: 684: 682: 678: 677: 675: 674: 669: 662: 657: 652: 643: 638: 632: 630: 626: 625: 623: 622: 617: 608: 602: 600: 596: 595: 593: 592: 587: 581: 579: 575: 574: 572: 571: 562: 557: 541: 532: 526: 524: 520: 519: 513: 498: 495: 494: 487: 480: 472: 466: 465: 459: 454:Programa SATEC 449: 448:External links 446: 443: 442: 418: 394: 380: 379: 377: 374: 357: 354: 353: 352: 349: 343: 340: 337: 329: 326: 325: 324: 321: 318: 312: 306: 303: 300:parallelepiped 284: 281: 269:microsatellite 251: 250: 247: 246: 243: 242: 239: 233: 232: 229: 223: 222: 219: 213: 212: 209: 203: 202: 199: 193: 192: 189: 183: 182: 177: 173: 172: 167: 163: 162: 158: 157: 154: 153: 150: 149: 143: 139: 138: 132: 128: 127: 110: 106: 105: 101: 100: 97: 96: 93: 92: 89: 85: 84: 79: 75: 74: 70: 69: 66: 65: 62: 61: 58: 54: 53: 50: 44: 43: 38: 34: 33: 27: 23: 22: 9: 6: 4: 3: 2: 1135: 1124: 1121: 1119: 1116: 1115: 1113: 1099: 1092: 1086: 1083: 1081: 1080:Ekspress AM22 1078: 1076: 1073: 1071: 1068: 1066: 1063: 1061: 1057: 1053: 1050: 1048: 1045: 1043: 1040: 1039: 1037: 1033: 1027: 1026: 1022: 1018: 1016: 1012: 1009: 1007: 1004: 1002: 999: 998: 996: 992: 986: 983: 981: 977: 974: 972: 969: 967: 966: 962: 960: 959:Resourcesat-1 957: 955: 954: 950: 948: 944: 941: 940: 938: 934: 928: 924: 920: 917: 915: 911: 907: 904: 902: 898: 895: 894: 892: 888: 882: 879: 877: 876:Progress M-48 874: 872: 869: 867: 863: 860: 858: 855: 853: 850: 848: 845: 844: 842: 838: 832: 829: 827: 824: 823: 821: 817: 811: 810:Cubesat XI-IV 807: 803: 799: 795: 791: 787: 783: 779: 778:Monitor-E GVM 776: 774: 771: 769: 766: 764: 760: 757: 755: 752: 750: 747: 745: 742: 740: 737: 735: 732: 729: 725: 722: 721: 719: 715: 709: 706: 704: 701: 698: 694: 691: 689: 686: 685: 683: 679: 673: 670: 668: 667: 663: 661: 658: 656: 653: 651: 647: 644: 642: 639: 637: 634: 633: 631: 627: 621: 618: 616: 612: 609: 607: 604: 603: 601: 597: 591: 588: 586: 585:Progress M-47 583: 582: 580: 576: 570: 566: 563: 561: 558: 555: 551: 547: 546: 542: 540: 536: 533: 531: 528: 527: 525: 521: 516: 512: 501: 493: 488: 486: 481: 479: 474: 473: 470: 463: 460: 455: 452: 451: 432: 428: 422: 408: 404: 398: 391: 385: 381: 373: 371: 367: 363: 350: 347: 344: 341: 338: 335: 334: 333: 322: 319: 317: 313: 311: 307: 304: 301: 297: 296: 295: 292: 290: 280: 278: 274: 270: 266: 262: 258: 248: 244: 240: 238: 234: 230: 228: 224: 220: 218: 214: 210: 208: 204: 200: 198: 194: 190: 188: 184: 181: 178: 174: 171: 168: 164: 159: 155: 151: 147: 144: 140: 136: 133: 129: 125: 111: 107: 102: 98: 94: 90: 86: 83: 80: 76: 71: 67: 63: 59: 55: 51: 49: 45: 42: 39: 35: 31: 28: 24: 20: 1097: 1019: 980:Chuang Xin 1 963: 951: 724:Mars Express 703:Hellas Sat 2 664: 590:Intelsat 907 550:SpaceHab RDM 543: 434:. Retrieved 430: 421: 410:. Retrieved 406: 397: 388:Wade, Mark. 384: 359: 331: 293: 286: 264: 256: 254: 187:Eccentricity 78:Manufacturer 26:Mission type 1060:Kosmos 2404 1056:Kosmos 2403 1052:Kosmos 2402 1006:Shen Tong 1 965:Soyuz TMA-3 866:Kosmos 2401 862:Kosmos 2400 852:Kosmos 2399 847:EchoStar IX 826:Opportunity 802:AAU-Cubesat 734:Kosmos 2398 666:Soyuz TMA-2 660:Kosmos 2397 231:100 minutes 217:Inclination 142:Launch site 116:2003-08-25Z 109:Launch date 88:Launch mass 1112:Categories 1047:Gruzomaket 953:Shenzhou 5 947:Horizons-1 436:2020-06-04 412:2020-06-04 403:"UNOSAT 1" 376:References 170:Geocentric 52:F20030822A 1015:Yamal-202 1011:Yamal-201 943:Galaxy 13 890:September 831:Rainbow 1 773:Orbview-3 749:Thuraya 2 708:Beidou 1C 655:AsiaSat-4 650:Galaxy 12 273:Brazilian 146:Alcântara 120:(planned) 48:COSPAR ID 1085:Tan Ce 1 1035:December 994:November 985:SERVIS-1 923:INSAT-3E 910:BILSAT-1 857:SCISAT-1 798:QuakeSat 728:Beagle 2 693:Hayabusa 646:INSAT-3A 578:February 530:Coriolis 298:Format: 283:Features 267:, was a 37:Operator 1070:USA-175 1065:USA-174 1042:USA-173 1001:FSW-3 1 976:CBERS-2 971:USA-172 936:October 927:SMART-1 914:STSat-1 901:Orion 5 897:USA-171 881:USA-170 871:Spitzer 763:BSAT-2c 697:Minerva 641:USA-169 620:USA-168 606:USA-167 565:USA-166 545:STS-107 539:CHIPSat 523:January 427:"SATEC" 356:Mission 328:Payload 308:Orbit: 261:English 241:Planned 148:VLS Pad 114: ( 32:orbiter 1075:Amos-2 1025:IGS-2B 1021:IGS-2A 919:e-Bird 906:UK-DMC 840:August 806:CanX-1 794:Cute-I 786:DTUSat 782:MIMOSA 754:Spirit 688:GSAT-2 615:IGS-1B 611:IGS-1A 569:XSS-10 535:ICESat 515:2004 → 500:← 2002 362:UNOSAT 227:Period 176:Regime 131:Rocket 739:AMC-9 672:GALEX 629:April 599:March 560:SORCE 462:SATEC 390:SATEC 366:VLS-1 289:VLS-1 265:SATEC 263:) or 237:Epoch 135:VLS-1 30:Earth 17:SATEC 819:July 790:MOST 717:June 508:2003 277:INPE 255:The 82:INPE 41:INPE 681:May 554:EDO 346:GPS 316:rpm 221:15° 1114:: 1058:, 1054:, 1023:, 1013:, 978:, 925:, 921:, 912:, 908:, 899:/ 864:, 808:, 804:, 800:, 796:, 792:, 788:, 784:, 780:, 761:, 648:, 613:, 567:, 552:, 537:, 429:. 405:. 372:. 137:V3 945:/ 730:) 726:( 699:) 695:( 556:) 548:( 491:e 484:t 477:v 439:. 415:. 191:0 126:) 118:)

Index

Earth
INPE
COSPAR ID
INPE
Alcântara accident
VLS-1
Alcântara
Geocentric
Heliosynchronous
Eccentricity
Perigee altitude
Apogee altitude
Inclination
Period
Epoch
English
microsatellite
Brazilian
INPE
VLS-1
parallelepiped
Heliosynchronous
rpm
GPS
UNOSAT
VLS-1
Accident of Alcantara
SATEC
"UNOSAT 1"
"SATEC"

Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.