Skip to main content

Earth Station Antenna

There are many types for earth station antenna, which are :

1. Prime Focus Feed
  • Most popular due to its excellent efficiency (approximately around 62%)
  • Because of its relatively large surface, the prime focus antenna is less sensitive to small directional deviations and there is a better chance of receiving signals outside the normal footprint.
  • Usually limited up to 4.5 mtr diameter
  • Sometimes problem with OMT adjustment for "prima" Cross-Polar Isolation (CPI) characteristics
  • Because of the LNB is mounted centrally, a lot of the incoming signals are blocked by the LNB on the way to the antenna surface.


2. Offset Feed
  • Better efficiency due to reduction of Feed (and spars) "blocking"
  • Simple to deploy, usually to Fly-away or Transportable SatCom terminals
  • Much easier to adjust in achieving very accaptable Cross-Pol Isolation (CPI)
  • Due to its simple construction, while satisfying the requaired ruggedness of Feed support, normally these are produced max on 3.8 mtr diameter
  • Usually the offet degree is 22 which means that the beam comes off the dish at an offset angle of 22 deg

3. Cassegrain / Gregorian Feed
  • This type of Feed is usally used for Antenna's aperture larger than 4.5 mtr
  • Very safe (in radiation aspects)
  • Relatively very convenient in CPI set-up
  • Cassegrain antenna is a double reflector system which works on the principle of Cassegrain optical telescope
  • The main advantages of Cassegrain antenna are a reduction in the axial dimensions of the antenna just as in optics and a greater flexibility in the design of the feed system
  
 
  •  The difference between Cassegrain and Gregorian is on the secondary reflector. Cassegrain is convex secondary reflector while Gregorian is concave secondary reflector
 
 
Example of Gregorian type Antenna

Comments

  1. Good info. I have a question.
    Do you know if the applications on cell phone give sattelite position relative to true North or magnetic North or the set angle of the dish itself with its correction (22 degree)? Thanks

    ReplyDelete

Post a Comment

Popular posts from this blog

Satellite Communication : Transmission Bands

A satellite link is a radio link between a transmitting earth station and receiving earth station through a communications satellite. A satellite link consists of one uplink and one downlink; the satellite electronics (i.e., the transponder) will remap the uplink  frequency to the downlink frequency. The transmission channel of a satellite system is a radio channel using a direct-wave approach, operating in at specific RF bands within the overall electromagnetic spectrum as seen below : The table below shown some key of physical parameters of relevance to satellite communication,  The frequency of operation is in the super high frequency (SHF) range (3-30 GHz). Regulation and practice dictate the frequency of operation, the channel bandwidth, and the bandwidth of the subchannels within the larger channel. Different frequencies are used for the uplink and for the downlink. Frequencies above about 30 MHz can pass through the ionosphere and

Satellite Communication - Part 4 (CPI)

Cross Polar Isolation (CPI) In installation and pointing/peaking antenna, Orthogonal Mode Transducer (OMT) must be set to be as precise as possible to get the best CPI value. above is picture of OMT Feed assembly include with BUC and LNB The minimum value for CPI is 30 dB (better will be good) in Linier Polarized Antennas. The reason is for our receive (Rx)-side as not to get interferenced (distrubed) by other (polarity) Down-Link users, therefore our transmit (Tx) shoild as well not interfere other users that operates at 90 deg (Orthogonal) Polarization. Note : In LH/RH Circular Polarizations, usually CPI of 27dB (=AR of 1.09) is acceptable enough. picture above is careless/miss-aligned OMT setting

Satellite Communication - Part 1

In this occasion, i want to share about Satellite communication. First, please look at the picture below, Planets of our Solar System God created Moon as our Earth satellite. In order to broading our communication, people tend to use artificial satellite for communication. Based on orbits, these are the type of satellites : Low Earth Orbit (LEO)              Height : 750-2500 Km,       Period : 2 - 2.5 hours Medium Earth Orbit (MEO)       Height : 7500-10000 Km,   Period : 4.5 - 6 hours High Earth Orbit (HEO)             Height : 15000-20000 Km, Period : 11-12 hours Geo-Stationary Orbit (GSO)      Height : 36000 Km,             Period : 24 hours Incline Orbit Satellite (drifting > 0.1 deg. N-S and E-W) Polar (mostly very eliptical) orbit satellite "in this purpose of satellite communication, I will focus in Geo-Stationary Orbit (GSO)" If we talk about GSO, we must mention this name, Arthur C. Clarke, a Science-Fictionist, which wrote : "a Satellite