Satellite Downlink Interference Information Sheet

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Courtesy of Spacecom Systems

Jump to: Natural RFI Examples Man-made RFI Examples Summary

Preface

Throughout its history, satellite communication has always been challenged by external noise sources. From natural occurrences, such as background radiation from the movement of particles in space or manmade sources like automobile ignition coils, RFI (Radio Frequency Interference) is everywhere. In addition, although universal, it is not equally distributed. RFI can be more pronounced in certain geographic locations or in certain frequency bands. Additionally, man-made RFI is becoming more prevalent as electronics products become a bigger part of our everyday lives. Because of the potential for RFI to cause degradation to vital satellite delivered information, our engineers have prepared this information sheet designed to inform you about RFI and how to overcome it.

What is RFI?

In its basic form, RFI is reception of any signal other than the one that is intended, and as described above, is both natural and man-made. This "unintended reception" can result from any one or any combination of many different sources.

Examples of natural RFI experienced at downlink sites are:

  1. Background Radiation - Random electron motion throughout the universe is measurable and contributes to thermal noise. Thermal noise in space is generated by the movement of charged particles through magnetic fields. Thermal noise in the atmosphere is compounded by re-radiation of any existing noise present. Both of these can contribute from 3 to 13 degrees Kelvin of "noise" to a communication link depending on the frequency of the link. This effect of thermal noise against a relatively low-level satellite signal can be significant.

  2. To minimize effects of this type of noise, satellites have higher power transponders and amplifier manufacturers design cooler noise temperature LNB's. A good communication link design can overcome the effects of these noise sources.
  3. Solar flares - Excessive solar radiation can damage spacecraft.
  4. Faraday rotation - This phenomenon is linked to the 11-year rotation of the sun. It affects linear, but not circularly polarized signals. The effects are more severe at lower frequency regions such as C-Band and are usually not noticeable at Ku-Band frequencies. US Domestic C- and Ku-Band satellites are linearly polarized, and transmit, as well as receive, horizontal and vertical polarities. The two polarities on a satellite are isolated from each other by 30dB (average), and enable the spacecraft to utilize a sharing scheme called frequency reuse. During periods of Faraday rotation, as the satellite signal passes through the atmosphere, it becomes de-polarized causing undesirable reception of the opposing polarity.

  5. To minimize or eliminate these effects, satellite users, like SpaceCom, attempt to ensure there are no other reused frequency signals on the opposing polarity, as well as choose a satellite location that offers a shorter path through the atmosphere.

  6. Rain Fade - Rain fade is a single term for many conditions regarding degradation due to water droplets along the reception path. The effect of a high frequency signal passing through rain can cause signal attenuation and accounts for the majority of the problems associated with rain fade. However, rain is not the sole source of the problem. Moisture laden clouds (as those associated with rain) extend up through the atmosphere sometimes reaching altitudes of 75,000 feet. By the time a signal passes through a cloud system, it can be attenuated by as much as 1 dB. In addition to this phenomenon, rain can absorb and attenuate signals even further as well as depolarize them and add unwanted thermal noise. Moreover, water droplets on a feed horn window cause detrimental effects too.

  7. It is important to know that when it comes to rain fade effects, higher frequency signals like Ku-Band degrade faster, harder, and longer than their lower frequency C-Band counterparts.

    There are several ways to overcome the effects of degradation due to water. For constant rate transmission, ample power from the satellite is required to maintain adequate fade margin, i.e., FM Cubed. If the power must remain constant, and bandwidth is available, then FEC or other error correction techniques can be employed. Designers of the satellite link play an important role in determining the applicable transmission scheme for the desired result. As for the user, larger antennas generally do not offer much protection.

  8. Sun Fade - Twice a year, during the vernal and autumnal equinox's, the sun lines up directly behind the satellite. Thermal noise created by the sun rivals, and often overpowers, a satellite's output.

  9. As with rain fade, sun fade can be overcome with link design which makes use of adequate power and/or modulation techniques like those employed in FM Cubed and HyperCubed.

Examples of man-made RFI experienced at downlink sites are:

  1. Unintentional radiators - electric shavers, light switches, automobile ignition coils and spark plugs, fluorescent lights, computers, and power convening units. These devices as well as many others not classified as transmitters can prove to emit destructive RFI.

  2. It is recommended that a receive system is shielded and any unintentional radiators are removed from the general area.
  3. Intentional radiators - walkie talkies, amateur radio, cellular or PCS phones, terrestrial microwave, other satellites, same satellite, and paging transmitters. Many of these radiators either share or abut frequencies dedicated to satellite communication. Without careful coordination RFI could be a continuous problem.
  • Walkie talkies, amateur radio, cellular or PCS phones operate near, but usually never in the bands associated with satellite C and Ku-Band downlinks including L-Band signals from an LNB. However, close physical proximity to and relative high power of these radiators can cause amplifiers in LNB’s and receivers to become overloaded, effectively pushing the desired signal out of the way.

  • Keeping these emitters away from the downlink is an effective means of eliminating the RFI.

  • Terrestrial microwave has no direct frequency related threats to domestic Ku-Band spectrum, but C Band is another matter. C-Band satellite receive systems must co-exist and share frequencies with terrestrial microwave radio paths. Both the satellite and microwave systems share a portion of the same C-Band frequency spectrum. When a signal is received from both a satellite and a microwave source at the same frequency, the receiver has no way to determine which signal is to be ignored. This can cause problems ranging from reduced quality of reception to total loss of signal depending on the severity of the interference.

  • In order to minimize the possibility of interference from microwave paths, C-Band Fm Squared was engineered to fit into a mostly interference-free portion of the spectrum. This has proven to be an effective method of dealing with terrestrial microwave interference. Should the interference be so strong that the technology alone is not sufficient, in-line filters have proved successful in reducing the interference to acceptable levels.

  • Other satellites can be picked-up along with the desired satellite. Since satellites are spaced 2 degrees from each other, it is possible for a single antenna to receive two or more satellites simultaneously. To alleviate this problem, the space segment provider tries to ensure the adjacent satellites do not use the frequency spectrum occupied by its signal.

  • Currently, Hughes and AT&T strive to maintain this arrangement for our FM Cubed, HyperCubed, and FM Squared signals. Individual downlinks can prevent or reduce adjacent interference by selecting the largest 2-degree compliant antenna possible and ensuring it is assembled and mounted per the manufacturer's instruction.

  • The same satellite can interfere with the desired signal due to cross-polarization problems. These problems could be in either the uplink and or downlink chain.

  • To minimize or prevent same satellite RFI, satellite providers try to ensure cross-polarized signals are eliminated or are not objectionably unbalanced. Therefore, the feed horns of both uplink and downlink dishes are aligned to provide 30dB of isolation or better.

  • Paging transmitters operating near the L-Band region affect signals traveling from the LNB to the receiver. This problem is most commonly seen at shared paging transmitter sites that have multiple transmitters active at the same time. If the right combination of carrier frequencies occurs, harmonics that are at the L-band frequency range can be generated.

  • To reduce this type of interference, shielding the device receiving the interference should be investigated. Typically either the LNB, cabling, or the receiver should be examined.

    Summary:

    RFI is prevalent in satellite systems; nonetheless, with proper planning and implementation satellites are a proven technology for distributing vast amounts of information. The policies and practices by the FCC, satellite operators, satellite vendors, and end-users help ensure RFI issues remain at a minimum.

    Please contact Salem Music Network at 615-367-2210 if you have any questions regarding the interference information.

    Also, please check out Spacecom's Technical Bulletins section on their site for updated information.


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