Attachment Attachment

This document pretains to SES-LIC-20120210-00162 for License on a Satellite Earth Station filing.

IBFS_SESLIC2012021000162_938586

                         RF RADIATION HAZARD ANALYSIS
                                   Exhibit #B

Antenna Dia. (D)=1.2 Meters 3.937 Feet
Antenna Surface Area (SA)=1.131 sq meters
Subreflector Dia. (DS)=N/A (prime focus offset)
Subreflector Surface Area (AS)=N/A (prime focus offset)
KU Wavelength at 14.250 GHz (LAMBDA)=.0211 meters
Power at output of HPA flange=19.294 dB
Path Loss to OMT (IL)=.55 dB
Power at OMT Flange (P)=74.889 watts
Antenna Gain at 14.250 GHz (G)=43.5 dBi
Antenna Gain given in Power Ratio (GES)=2.239E+04
Antenna Aperture Efficiency (N)=.6981

Region                                 Radiation Level         Hazard Assessment
Far Field (RF) 40.948 m 134.35 ft       7.957 mW/cem sq        Potential Hazard
Near Field (WF) 17.062m 55.979 ft      18.49 mW/cm sq          Potential Hazard
Transition Region (RT)                 equal to or less than   Potential Hazard
    Ru<Rt<Rf                           18.49 mW/cm sq
Between Main Reflector and             N/A
    Subreflector (WS)
Main Reflector Region (WM)             13.243 mW/em sq         Potential Hazard
Power Density Between Reflector        6.622 mW/cm sq          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 toward the satellite that it is pointed at. The Area
occupied by the general public will not exceed the ANSI limit of 1 mW cm sq. because the
antenna is mounted on top of the truck, which is at least 8 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

Note: See Exhibit #Ba for how the above calculations were made.


                                    Exhibit Ba Analysis of Non—lonizing Radiation

Antenna Diameter, (D)=..........22020000002. 2.               D:=1.2             meters          D—3.281=3.937       Feet
                                                                          DD
Antenna Surface Area, (Sa)= .................222.             Sa :=   n £200000002
                                                                                          Sa=1.131     sq meters

Subreflector Diameter, (Ds)=..........00022.222222.2.         Ds :=0                 cm          Ds—.3937=0           Inch‘s


Area of Subreflector, (AS)=................2.02.22222.        As :=1                                           sq cm

Center Frequency, (Cf)=.................0.0.c ...             CF := 14.250             GHz
Wavelenght at (Cf), (Lambda)=....................             Lambda :=.0211 meters
                                                              C—Band=.049 Ku—Band=.0211
Transmit Power at HPA or VPC Flange, (P1)=..                  P1 =80             watts P2:=log(P1)—10 P2=19.031d0B
Path Loss from HPA or VPC to OMT, (Lossy=..                   Loss := .55            dB
                                                              P3 =P2— Loss                  P3 =18.481     OMT Pwr in dB
Power at OMT, (PJ=..........00..0000000c e                         p3

                                                              P:=10"                        P = 70.484     OMT Pwr in watts
Antenna Gain at (Cf), (Gain)=...............llcll.            Gain =43.5                  dBi
                                                                            Gain
Antenna Gain Converted to Power Ratio, (Ges).                 geg = 10 ‘°                 Ges=2.23910            Ratio

Antenna Aperture Efficiency, (M)=.............2.22222.        n ‘=.6981



Far Field (Rf)=     Rf:= «60(DD)            Rf=40.948         meters                 Rf3.281=134.35           Feet
                          Lambda
      .                .                          Ges—P
Far Field Pwr Density (Wf)=             Wf :=———————.1 Wf=7489                                  mw sq cm
                                              41 —(RERA)
          .                          DD
Near Field (Rn)=           Rn i= ———————           Rn =17.062         meters               Rn—3.281=55.979         Feet
                                4 Lambda
          .                 .                 _   1l6nP
Near Field Pwr Density (Wna)=             Wn :=————— .1        Wnn =17.403 mw sq cm
                                              1—(D D)

Transition Region (Rt)= Rt:=Wn—1                  Rt=17.403      mw sq cm (Equal to or less then)

Pwr Density at Sub Reflector (Ws)=             N/A (no sub reflector)                             mw sq cm

Main Reflector Region Pwr Density (VWm)=                  Wm:= gs?l Wm = 12.464 mw sq cm
                                                                  a

              .                 .                                                     P
Pwr Density between main reflector and ground (Wg)= Wg := S—l Wg =6.232                                       mw sq cm
                                                                                      a



Document Created: 2012-02-08 10:11:10
Document Modified: 2012-02-08 10:11:10

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