Attachment Attachment 1

This document pretains to SES-LIC-20120208-00149 for License on a Satellite Earth Station filing.

IBFS_SESLIC2012020800149_938538

                                       RF RADIATION HAZARD ANALYSIS
                                                  Exhibit A


Antenna Dia. (D) = 2.4 Meters (7.874 feet)
Antenna Surface Area (SA) = 4.523893 meters2
Subreflector Dia. (DS) = 51.435 cm 20.25 inches
Subreflector Surface Area (AS) = 2077.817 cm2
KU Wavelenght at 14.250 Ghz ( )= 0.0211 meters
Power at output of VPC flange = 28.129 dB
Path Loss to OMT (IL) = 1.1 dB
Power at OMT Flange (P) = 504.561 watts
Antenna Gain at 14.250 Ghz (G) = 49.4 dBi
Antenna Gain given in Power Ratio (GES) = 0.87096E+05
Antenna Aperture Efficiency (N)=0.679


Region                                          Radiation Level                   Hazard Assessment

Far Field (RF) 163.79 m (537.368 ft)            13.035 mW/cm2                     Potential Hazard

Near Field (WF) 68.24 m (223.917 ft)            30.292 mW/cm2                     Potential Hazard

Transition Region (RT)                           30.292 mW/cm2                    Potential Hazard
        Ru<Rt<Rf

Between Main Reflector and                      485.664 mW/cm2                    Potential Hazard
       Subreflector (WS)

Main reflector Region (WM)                      22.306 mW/cm2                     Potential Hazard

Power Density Between Reflector                 11.153 mW/cm2                     Potential Hazard
       and ground


Conclusion:    Based on the above analysis, harmful areas of Radiation do exist in areas around the antenna and in
               the path of the antenna pointed toward the satellite. The area occupied by the general public will not
               exceed the ANSI limit of 1.0 mW/cm2 because the antenna is mounted on top of the truck, which is at
               lease 10 feet above the ground, and safety increases with look angles used by the Satellites in the
               United States on Dom. Sat. Arch. The SNG will be marked with the standard radiation hazard
               warnings, and on the antenna itself. The warning signs will warn personnel to avoid the area around
               and in front of the reflector when the transmitter is operating. To ensure compliance with safety
               limits, the earth station transmitter will be turned off and marked to remain off whenever maintenance
               and repair personnel are required to work in the areas of potential hazard as defined in the above
               study. Additionally, the earth station personnel will be trained to insure that the antenna path is clear
               at all times while the transmitter is in operation. The only access to the roof of the truck, is a stored
               ladder which will only be used when the transmitter is off. Therefore, the roof is not accessible to the
               general public. See Page 2 for calculations.


                                      RF RADIATION HAZARD ANALYSIS
                                                 Exhibit A
                                                  Page 2


                                       Analysis of Non-Ionizing Radiation

Antenna Diameter, (D) =                                 D = 2.4 meters (7.874 ft)
Antenna Surface Area, (Sa) =                            Sa = D2/4 = 4.524 meters2
Subreflector Diameter, (Ds) =                           Ds = 51.435 cm (20.25 inches)
Area of Subreflector, (As) =                            As = Ds2/4 = 2.078x103 cm2
Center Frequency, (Cf) =                                Cf = 14.250 GHz
Wavelength at (Cf), ( ) =                                = 0.0211 meters
                                                        C-Band=0.049 Ku-Band=0.0211
Transmit Power at HPA or VPC Flange, (P1) =             P1=650 watts, P2=log(P1) *10 = 28.129 dB
Path Loss from HPA or VPC to OMT, (Loss) =              Loss = 1.1 dB
                                                        P3=P2-Loss, P3=27.029, OMT Pwr in dB
Power at OMN, (P) =                                     P = 10P3/10= 504.561, OMT Pwr in watts
Antenna Gain at (Cf), (Gain) =                          Gain = 49.4 dBi
Antenna Gain Converted to Power Ratio, (Ges) =          Ges = 10Gain/10=8.71x104, Ratio
Antenna Aperture Efficiency, (n) =                      n = 0.679




Far Field (Rf) =                                        Rf = 0.60 (D2)/ = 163.791 meters (537.4 ft)
Far Field Pwr Density (Wf) =                            Wf = [Ges x P/4 (Rf2)] x 0.1 = 13.035 mw/cm2
Near Field (Rn) =                                       Rn = D2/4 = 68.246 meters (223.917 ft)
Near Field Pwr Density (Wn) =                           Wn = [(16 x n x P)/ D2 ]x0.1=30.292 mw/cm2
Transition Region (Rt) =                                Rt 30.292 mw/cm2
Pwr Density at Sub Reflector (Ws) =                     Ws = [(2 x P)/As] x 1000 = 485.664 mw/cm2
Main Reflector Region Pwr Density (Wm) =                Wm = [(2 x P)/Sa] x 0.1 = 22.306 mw/cm2
Pwr Density between main reflector and ground (Wg) =    Wg =[P/Sa] x 0.1 = 11.153 mw/cm2


6.46 METERS                   FIGURE 1

                      KTVX(TV)
                      SALT LAKE CITY, UTAH
5.26 METERS




              °   °



Document Created: 2012-02-08 11:08:20
Document Modified: 2012-02-08 11:08:20

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