Attachment RF Radiation Analysi

This document pretains to SES-LIC-20080818-01065 for License on a Satellite Earth Station filing.

IBFS_SESLIC2008081801065_659019

                        F RADIATION HAZARD ANALYSIS
                                 Exhibit #1

Antenna Dia. (D)=2.4 Meters 7.874 Feet
Antenna Surface Area (SA)#4.523893 sq meteors
Subreflector Dia. (DS)=§51.435 ocm 20.25 Inches
Subreflector Surface Area (AS)=«2077.81 7 sq cm
KU Wavelength at 14.250 GHz (LAMBDA)s.0211 meters
Power at output of HPA flange=25.441 dB
Path Loss to OMT (IL)=.6 dB
Power at OMT Flange (P)=304.837 watts
Antenna Gain at 14.250 GHz (G)=49.4 dBi
Antenna Gain given in Power Ratio (GES)=.87096E+05
Antenna Aperture Efficiency (N)=.679

Region                             Radiation Level      _HazardAssessment
Far Field (RF) 163.79 m 537.368 ft         7.875 mW/icm sq Potential Hazard
Near Fleld (WF) 68.24m 223.917 ¢    18.301 mWi/icm sq Potential Hazard
Transition Region (RT)        equal to or less than   Potential Hazard
   RuSRt«<Rf                        18.301 mWi/icm sq Potential Hazard
Between Main Reflector and             ©2093.421 mWicm sq Potentlial Hazard
   Subreflector (WS)
Main Reflector Region (WM)              18.477 mWiecm sq Potential Hazard
Power Density Between Reflector           6.738 mWicm sq Potential Hazard
   and Ground
Power Density 2.4 meters off axis
    from center of beam                  2.808 mW/icm sq No Hazard
Concluslon: 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, but safe when 2.4 meters off axis from the antenna look angle. The Area occupled
by the general public will not exceed the ANSI limit of 5§ mW em sq. because the
antenna is mounted on top of the truck, which is at least 9 feet above the ground, and .
safety Increases with loock 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 trangmitter
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 and not accessible by the general public,

Note: See Exhibit #2 for how the above calculations were made.


                            Analysis of Non—lonizing Radiation Exhibit
Ant@nn@ DI@Met@r, (D)S........,....0 0c ecrrerems »             D —2.4       meters     D:3.281 =7.874      Feet

Antenna Surface Area, (Sa)® ................... m               S0 -x-%-g        Sa =4.524    sq meters

Subreflector Diameter, (OD#8)=.........................         Ds     ~51.435 ocm      Ds.3937=20.250        Inch‘s

Ar®® Of SUDT@fI@CIOF, (AS}®.............ccsclccen               As > ,‘.9'4‘)‘        As =2.07810 sq om
Cant@er FF@qUONCY, (CT)Z..))...0....0.00.m mm                   CF ©14.250 GHz
Wavelenght at (Cf), (Lambda)=................. o                Lambda ~.0211 meters
                                                                C—Band=.040 Ku—Band=.0211
Transmit Power at HPA or VPC Flange, (P1)=..                    P      350
                                                                        &  watts P2 =log(P1) 10 P2 =25.441             dB
Path Loss from HPA or VPC to OMT, (Losg)=..                     Loss *.6       dB
                                                                P3 «P2 — Loss         P3 #24.84|   OMT Pwr in dB
Power at OMT, (P)=...............o en                                   p3
                                                                P srg!®               P =304.837   OMT Pwr in watts
Antenna Gain at (CT), (Ga@in)®...................ov}            Gain +49.4       dBi
                                                                          Cxi
Antenna Gain Converted to Power Ratio, (Ge§):                    5,, . 10*’_"’9 Ges =8.71°10°            Ratio

Antenna Aperture Efficiency, (n)®...................            n 5.679


Far Field (RFQ)#®    Rf   = '-61:95%?-      Rf = 163.791        meters        Rf:3.281 = §37.4       Feet


Far Field Pwr Density (WQ=            Wf—= ~~-q-°-?g—-—-.l Wf = T.875                  mw sq m
                                              4: x( RFRF)

Near Flald (Rn)®             ~34gihy,              Rn=68,246 metere                  Rn3.281=223.917 Feet
Near Field Pwr Density (Wn)=             Wnn = 1-§"-"-'~P~~.l     Wa = 18301 mw sq cm
                                              *{DD)
Transition Region (Rt)s Rt = Wal                 Rt=18.301           mw sq cm (Equal to or lesgs then)

Pwr Density at Sub Reflector (We)=
                                                   2P
                                                W3 > As 1000          Ws =293.421         mw sq ¢m

Main Reflector Region Pwr Density (Wm)s                   Wm 2S'Pl Wm = 13.477 mw sq em


Pwr Density between main reflector and ground (Wg)= We                         §2v.l We =6.738       mw sq cm

Pwr Density between reflector eage and ground (WM)=                     W1     We
                                                                                6      WI=2,808      mw sq cm



Document Created: 2008-08-18 10:19:02
Document Modified: 2008-08-18 10:19:02

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