Attachment RADHAZ

This document pretains to SES-LIC-20140430-00327 for License on a Satellite Earth Station filing.

IBFS_SESLIC2014043000327_1044331

                                 EXHHIBIT
                       RF RADIATION HAZARD ANALYSIS
Antenna Dia. (D) = 4.5 M
Antenna Surface Area (SA) = 15.9 Sq M
Wavelength at 6.175 GHz (2) = 0.0486 M
Power at output of HPA flange (P2) =28.45 dBm
Path Loss to OMT (IL) = 1.92 dB
Power at OMT Flange (P) = 450 watts
Antenna Gain at 6.175 GHz (G) = 46.4 dBi
Antenna Gain given in Power Ratio (Ges) = 43,652
Antenna Aperture Efficiency (N) = 0.52

Region                        Distance             Radiation Level      Hazard
                                                                        Assessment
Far Field (WF)                (Rf) 250 m           2.5 mw/cm*            Potenial Hazard
Near Field (Wn)               (Rn) 104 m           5.88 mw/icm*          Potenial Hazard
Transistion Region            Rn<(Rt)<Rf           <5.88 mw/icm*         Potenial Hazard
Main Reflector (Wm)                                5.66 mw/icm*          Potenial Hazard
Power Density between                              2.83 mw/cm*           Potenial Hazard
Reflector and Ground (Wg)
Far Field Off Axis (WF)                            0.025 mwicm*         Meets ANSI
Near Field Off Axis (WN)                           0.059 mw/cm*         Meets ANSI


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 %0 q
feet above the ground, and safety increases with look angles used by the Satellites in
the United States on Dom. Sat. arch. The areas on the ground and behind the antenna
are 100 times less power (20 dB) when at a min. of the dia. of the reflector, this is
reflected in the Off Axis figures as seen above (WF) & (WN). 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 and not accessible by the general public.

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


                                   SXHIGI
                       ANALYSIS OF NON—IONIZING RADIATION


Antenna Diameter (D) = 4.5 M

                                   DZ

Angtenna Surface Area (Sa) = ”[T} = 15.9 Sq M


Center Frequency (Cf) = 6.175 GHz

Wavelength at Center Frequency(2) = 0.0486 M

Maximum Transmit Power in Watts (P1) = 700 W

Maximum Transmit Power in dB (P2) = 10Log(P1) = 28.45 dBm

WIG loss from Transmitter to Feed, (IL) = 1.92 dBm

Total Feed Input Powerin dB (P3) = P2—Loss = 26.53 dBm

Total Feed Input Power in Watts (P) = 10‘ = 450 W

Antenna Isotropic Gain (G) = 46.4 dBi

Antenna Gain Converted to Power Ratio (Ges) = 10%= 43,652

Antenna Nominal Efficiency (N) = 0.60



Far Field (RF) = 0—6&”——) =250 M
                       2




Far Field Power Density (WB = °x 0.1 = 2.5 mwiem*
                               Ar(Rf)‘

Near Field (Rn) = % =104M
                   2




Near Field Power Density (Wn) = [%%1]0.1 = 5.88 mwiom*


Transistion Region (Rt) = Wn = 5.88 mwfcm*


Main Reflector Region Power Density (Wm) = [zv"
                                            80
                                                ]0.1   = 5.66 mwicm*


Power Density between Main Reflector and Ground (Wg) = [—}f—}o.l =2.83 mwiem*
                                                        Sa

Far Field Off Axis (WF) = WH(0.01) = 0.025 mwicm*

Near Field Off Axis (WN) = Wn(0.01) = 0.059 mw/cm*



Document Created: 2014-04-24 16:22:39
Document Modified: 2014-04-24 16:22:39

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