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A project log for Disabling satellite systems intruding aircraft.

All systems of satellites manufactured in the world contains critical vulnerabilities that could be exploited to stop military operations an

jose-pedro-r-a-ribeiroJose Pedro R. A. Ribeiro 12/13/2015 at 18:250 Comments

Communication Satellite Systems

  • Basic concepts
  • Orbit satellites
  • Connections satellite
  • Access to satellites
  • Satellite Segment
  • Ground segment
  • Satellite Series
  • applications
    Fixed Communications (FSS Fixed Satellite Service)
    Broadcasting (BSS Broadcasting Satellite Service)
    Mobile Communications (MSS Mobile Satellite Service)
    - Aeronautical - Maritime - Terrestrial
    amateur radio
    Navigation (location)
    Earth observation and atmosphere
    - Weather - Remote sensing
    Use
    business
    private
    Military
    experimental
    scientific
  • • Situação actual Satélites lançados e operacionais (Dezembro 2000) – 2 490 satélites lançados com sucesso no período de 1980-2000 – 570 satélites operacionais (mínimo estimado) Organizações responsáveis – lançamento de satélites de órbita alta  URSS / CEI Molniya (1960), Proton (1967)  EUA Atlas (1962), Titan (1965), Delta (1972), STS-Shuttle (1981)  China Longa Marcha (1975)  Europa Ariane (1979)  Japão NASDA (1981) – operação de sistemas  operadores específicos internacionais: Intelsat, Inmarsat, Eutelsat, Astra, Iridium  operadores tradicionais de redes de telecomunicações – regulamentação  organismos internacionais UIT-R (Sector de Radiocomunicações)  organismos nacionais Portugal - Anacom tendências gerais: globalização privatizaçao.
  • Orbit satellites them
    Types of orbits
    GEO (Geosynchronous Earth Orbit): circular equatorial geosynchronous orbit
    - Revolution period: 23 h 56 m 4.091 s
    - Average altitude: 35,786 km
    LEO (Low Earth Orbit): circular orbit of low altitude
    - Typical altitude: 500 - 1500 km
    - Revolution period 1h 30m - 2h
    MEO (Medium Earth Orbit): circular orbit of average altitude
    - Typical altitude: 10,400 km
    - Revolution period of six hours
    HEO (Highly Elliptical Orbit): strongly elliptical orbit
    - Inclined elliptical orbit
    - Lowland perigee
    notable case: Molniya orbit
    Perigee: 1,000 km alt. Apogee: 39,000 km alt.
    period
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