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Lanzamientos De Satelites Notificados En 1974

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Lanzamientos De Satelites Notificados En 1974 This electronic version (PDF) was scanned by the International Telecommunication Union (ITU) Library & Archives Service from an original paper document in the ITU Library & Archives collections. La présente version électronique (PDF) a été numérisée par le Service de la bibliothèque et des archives de l'Union internationale des télécommunications (UIT) à partir d'un document papier original des collections de ce service. Esta versión electrónica (PDF) ha sido escaneada por el Servicio de Biblioteca y Archivos de la Unión Internacional de Telecomunicaciones (UIT) a partir de un documento impreso original de las colecciones del Servicio de Biblioteca y Archivos de la UIT. (ITU) ﻟﻼﺗﺼﺎﻻﺕ ﺍﻟﺪﻭﻟﻲ ﺍﻻﺗﺤﺎﺩ ﻓﻲ ﻭﺍﻟﻤﺤﻔﻮﻇﺎﺕ ﺍﻟﻤﻜﺘﺒﺔ ﻗﺴﻢ ﺃﺟﺮﺍﻩ ﺍﻟﻀﻮﺋﻲ ﺑﺎﻟﻤﺴﺢ ﺗﺼﻮﻳﺮ ﻧﺘﺎﺝ (PDF) ﺍﻹﻟﻜﺘﺮﻭﻧﻴﺔ ﺍﻟﻨﺴﺨﺔ ﻫﺬﻩ .ﻭﺍﻟﻤﺤﻔﻮﻇﺎﺕ ﺍﻟﻤﻜﺘﺒﺔ ﻗﺴﻢ ﻓﻲ ﺍﻟﻤﺘﻮﻓﺮﺓ ﺍﻟﻮﺛﺎﺋﻖ ﺿﻤﻦ ﺃﺻﻠﻴﺔ ﻭﺭﻗﻴﺔ ﻭﺛﻴﻘﺔ ﻣﻦ ﻧﻘﻼ ً◌ 此电子版（PDF版本）由国际电信联盟（ITU）图书馆和档案室利用存于该处的纸质文件扫描提供。 Настоящий электронный вариант (PDF) был подготовлен в библиотечно-архивной службе Международного союза электросвязи путем сканирования исходного документа в бумажной форме из библиотечно-архивной службы МСЭ. © International Telecommunication Union lanzamientos de satélites notificados en 1974 Esta lista integra los satélites artificiales lanzados en 1974; está basada en los datos proporcionados por las administraciones de telecomunicaciones, el Comité de Investigaciones Espaciales (COSPAR), el Goddard Space Flight Center (GSFC — Centro de Vuelos Espaciales Goddard) de la Administración Nacional de la Aeronáutica y del Espacio (NASA), de Estados Unidos, el Ministerio de Comunicaciones de la URSS, el Centre national d'études spatiales (CNES), de Francia, la Junta Internacional de Registro de Frecuencias (IFRB), uno de los cuatro organismos permanentes de la UIT, y en las informaciones publicadas por la prensa especializada. Los parámetros orbitales son los datos iniciales. No se han tenido en cuenta los fragmentos o secciones de los propulsores satelizados con los distintos artefactos. BOLETIN DE TELECOMUNICACIONES - VOL. 42 - IV/1975 COSHOS-654 1974 32A HOLNYA-2 (10) 1974 56A A COSHOS-655 1974 35A D HOLNYA-2 (11) 1974 102A C0SM0S-656 19 74 36A HOLNYA-3 (1) 1974 92A C0SH0S-657 1974 38A COSHOS-658 1974 41A C0SM0S-659 1974 43A N AEROS-2 1974 55A COSMOS-660 1974 44A DHSP 1974 15A ANS-1 1974 70A COSMOS-661 1974 45A DMSP 1974 63A ARIEL-5 1974 77A C0SM0S-662 1974 4 7A NNTS-1 1974 54A ATS-6 1974 39A COSMOS-663 1974 48A NOAA-4 1974 89A COSMOS-664 1974 49A COSMOS-665 1974 50A H COSMOS-666 1974 53A O B C0SM0S-667 1974 57A HAWKEYE 1974 40A COSMOS—668 1974 5 8A HELIOS-1 1974 97A C0SM0S-669 1974 59A OS CAR-7 1974 89B BIG BIRD 1974 85A COSMOS-670 1974 61A C0SH0S-671 1974 62A i S C0SM0S-672 1974 64A I C C0SM0S-673 1974 66A C0SM0S-674 1974 68A COSMOS-675 1974 69A INTASAT 1974 89C SALYUT-3 1974 46 A C0SM0S-628 1974 1A C0SM0S-676 1974 71A INTELSAT-IV F8 1974 93A SALYUT-4 1974 104A COSMOS-629 1974 3A C0SM0S-677 1974 72A INTERCOSMOS—11 1974 34A SAHOS-97 1974 7A COSHOS-630 1974 4 A COSHOS-678 1974 72B INTER COSRO S—12 19 74 86A SAHOS-98 1974 20A C0SM0S-631 1974 5A C0SM0S-679 1974 72 C SAMOS-99 1974 42A COSMOS-632 19 74 6A COSMOS-680 1974 72 D SAHOS-100 1974 65A COSMOS-633 1974 10A C0SH0S-681 1974 72E 1 SAN MAR CO—4 1974 9A COSMOS-634 1974 12A C0SM0S-682 1974 72 F L SKYNET-IIA 1974 2A COSKOS-635 1974 14A COSMOS-683 1974 72G SKYNET-IIB 1974 94A COSMOS-636 1974 16A C0SM0S-684 SHS-1 1974 33A 1974 72H LUNA-22 1974 37A COSMOS-637 1974 17A C0SM0S-685 SOYUZ-14 1974 51A 1974 73A LUNA-23 1974 84A COSMOS-638 1974 18A C0SM0S-686 1974 74A SOYUZ-15 1974 67A COSHOS-639 1974 19A CO SMOS-6 87 1974 76A SOYUZ-16 1974 96 A COSMOS-640 1974 21A C0SM0S-688 1974 78A SYMPHONIE 1974 101A COSHOS-641 1974 24A C0SM0S-689 1974 79A M COSMOS-642 1974 24B COSHOS-690 1974 80A T COSMOS-643 1974 24C COSHOS-691 1974 82 A i COSMOS-644 19 74 240 C0SM0S-692 19 74 87A HETEOR-16 1974 11A COSMOS-645 1974 24E C0SH0S-693 1974 88A HETEOR-17 1974 25A COSHOS-646 1974 24F COSMOS-694 1974 90A HE TEOR-1 8 1974 52 A TANSEI-2 1974 8A C0SM0S-647 1974 24G C0SH0S-695 1974 91A HETEOR-19 1974 83A C0SH0S-648 1974 24H C0SM0S-696 1974 95A METEOR-20 1974 99A COSMOS-649 19 74 27A C0SH0S-697 1974 98A HIRANDA 1974 13A w COSMOS-650 1974 2 8A COSMOS-698 1974 10DA HOLNYA-1 (27) 1974 23A C0SH0S-651 1974 29A C0SM0S-699 1974 1D3A HOLNYA-1 (28) 1974 81A COSMOS-652 1974 30A COSHOS-700 1974 105 A HOLNYA-1S 1974 60 A WESTAR-1 1974 22A COSMOS-653 1974 31A COSHOS-701 1974 106A HOLNYA-2 (9) 19 74 26A WESTAR-2 1974 75A País Denominación Frecuencia Núm ero Organización Perigeo Periodo Descripción Fecha Potencia del Observaciones internacional Lugar del Apogeo Inclinación de la cosmonave transmisor lanzamiento Cosm os-628 1974-1-A URSS 17 en ero 975 km 105 min Lleva aparatos científicos, sistema radioeléctrico para (PLE) 1026 km 83° mediciones precisas de elementos orbitales y sistema de radiotelemedida. Satélite de navegación Skynet-IIA 1974-2-A Reino Unido 19 enero 1074 km El vehículo espacial quedó inutilizado a causa de un fallo Ministry of 31 300 km 26,5° en el lanzamiento. Defence destinadc a una órbita (ETR) sincró nica sobre Se desintegró el 25 de enero de 1975 el Oce ano índico Cosmos-629 1974-3-A URSS 24 enero 202 km 89,4 min 19,995 MHz Llevaba aparatos científicos, sistema radioeléctrico para (PLE) 315 km 62,8° mediciones precisas de elementos orbitales y sistema de radiotelemedida. Satélite de reconocimiento y vigilancia. Regresó a la Tierra el 5 de febrero de 1974 Cosm os-630 1974-A74 URSS 30 enero 213 km 90 min Llevaba aparatos científicos, sistema radioeléctrico para (PLE) 367 km 72,9° mediciones precisas de elementos orbitales y sistema de radiotelemedida. Satélite de reconocimiento y vigilancia. Regresó a la Tierra el 13 de febrero de 1974 Cosmos-631 1974-5-A URSS 6 feb. 522 km 95,3 min Lleva aparatos científicos, sistema radioeléctrico para (PLE) 565 km 74,0° mediciones precisas de elementos orbitales y sistema de radiotelemedida. Satélite de navegación Cosm os-632 1974-6-A URSS 12 feb. 184 km 89,4 min Llevaba aparatos científicos, sistema radioeléctrico para (BAI) 333 km 65° mediciones precisas de elementos orbitales y sistema de radiotelemedida. Satélite de reconocimiento y vigilancia. Regresó a la Tierra el 26 de febrero de 1974 Sam os-97 1974-7-A Estados 13 feb. 132 km 89,9 min Satélite de reconocimiento y vigilancia. Ocean surveillance Unidos 404 km 110,4° system (OSS). USAF (W TR) Regresó a la Tierra el 17 de marzo de 1974 Tansei-2 (MS-T2) 1974-8-A Japón 16 feb. 288 km 121,85 min 136,725 MHz Lleva equipo experimental para el sistema magnético Instituto de 3238 km 31,2° 100 m W de control de actitud del satélite, sistema de medida del Ciencias (radiofaro) funcionamiento del equipo y sistema de telemedida Espaciales y Aeronáuticas 400,450 MHz (KSC) 100 m W (radiofaro intermitente) 1 BOLETÍN DE TELECOMUNICACIONES - VOL. 42-IVI1975 País Denominación Frecuencia Número Organización Perigeo Periodo Descripción Fecha Potencia del Observaciones internacional Lugar del Apogeo Inclinación de la cosmonave transm isor lanzamiento San Marco-4 1974-9-A Italia 18 feb. 243 km 96,3 min 136,74 MHz Objetivos: medir las variaciones diarias de la densidad de CRA 919,7 km 2,89° (transmisión de datos mediante la atmósfera neutra ecuatorial, su composición y tempe­ satélite esférico; diámetro: (SM) órdenes) ratura. 0,70 m; masa: 170 kg; 4 antenas de 0,485 m Se efectuará la correlación de estos datos con los de Explorer-51 para estudios de física de la termosfera Cosmos-633 1974-10-A URSS 27 feb. 280 km 92,2 min Llevaba aparatos científicos, sistema radioeléctrico para (PLE) 516 km 71° mediciones precisas de elementos orbitales y sistema de radiotelemedida. Se desintegró el 4 de octubre de 1974 M eteor-16 1974-11-A URSS 5 marzo 853 km 102,2 min Lleva aparatos meteorológicos, sistema radioeléctrico (PLE) 906 km 81,2° para mediciones precisas de elementos orbitales y sistema de radiotelemedida Cosmos-634 1974-12-A URSS 5 marzo 281 km 92,2 min Llevaba aparatos científicos. (PLE) 516 km 71,0° Se desintegró el 9 de octubre de 1974 Miranda (UK-X4) 1974-13-A Reino Unido 9 marzo Satélite científico. Lleva equipo para 5 experimentos: NASA 1) subsistema de control de orientación; satélite rectangular, estabilización (WTR) 2 ) sensor infrarrojos en el plano horizontal; tres ejes; altura: 0,835 m; anchura: 0,665 m; 3) sensor estelar un solo eje; masa: 93,4 kg; células solares 4 ) sensor albedo en el plano horizontal; 5 ) experimento para determinar la degradación de las células solares de silicio en órbita Cosmos-635 1974-14-A URSS 14 marzo 212 km 89,8 min 19,995 MHz Llevaba aparatos científicos, sistema radioeléctrico para (PLE) 350 km 72,9° mediciones precisas de elementos orbitales y sistema de radiotelemedida. Misión de reconocimiento fotográfico y vigilancia. Regresó a la T ierra el 26 de marzo de 1974 DMSP 1974-15-A Estados 16 marzo 780 km 101,5 min Satélite del Defense Meteorological Satellite Program Unidos 876 km 98,9° USAF (W TR) 2 Cosmos-636 1974-16-A URSS 20 m arzo 174 km 90,0 min Llevaba aparatos científicos, sistema radioeléctrico para (BAI) 409 km 65,0° mediciones precisas de elementos orbitales y sistema de radiotelemedida.
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