Attachment Cakhoun 2.4M RadHaz.

This document pretains to SES-LIC-20140218-00061 for License on a Satellite Earth Station filing.

IBFS_SESLIC2014021800061_1034542

                                  EXHHIBIT B
                        RF RADIATION HAZARD ANALYSIS

 Antenna Dia. (D) = 2.4 M
 Antenna Surface Area (SA) = 2.5 $q M
 KU Wavelength at 14.250 GHz (2) = 0.0211 M
 Power at output of HPA flange (P2) =27.78 dBm
 Path Loss to OMT (IL) = 0.79 dB
 Power at OMT Flange (P) = 500 watts
 Antenna Gain at 14.250 GHz (G) = 46.5 dBi (4 port antenna gain)
 Antenna Gain given in Power Ratio (Ges) = 44668
 Antenna Aperture Efficiency (N) = 0.60

 Region                           Distance                   Radiation Level   | Hazard
                                                     .                 _        Assessment____|
 Far Field (Wf)                   (Rf) 92 m                  21.0 mw/icm*       Potenial Hazard       |
 Near Field (Wn)                  (Rn) 38 m                  47.2 mwicm*        Potenial Hazard
  Transistion Region              Rn<(Rt)<RFf                <47.2 mwicm"       Potenial Hazard __|
| Main Reflector (Wm)                                        40.0 mwicm*        Potenial Hazard
| Power Density between                                  i 20.0 mw/icm?         Potenial Hazard
 Reflector and Ground (Wg) |                             |             _                    _
 Far Field Off Axis (WF)      1                              0.21 mwicm*        Meets ANSI
 Near Field OffAxis (WN)      j               _______|       0.47 mwicm*        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 10
 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.


                                 EXHIBIT Ba
                     ANALYSIS OF NON—IONIZING RADIATION


Antennia Diameter (D) = 1.8 M
                                          a 7
                                      )
                                          ~   d
Arfitenna Surface Area (Sa) = Jl’4 §=2,58qM



                                 —
                                              J



Center Frequency (Cf} = 14.25 GHz

Wavelength at Center Frequency(1) = 0.0211 M

Maximum Transmit Power in Walts (P1) = 600 W

Maximum Transmit Power in dB (P2) = 10Log(P1) = 27.78 dBm

WIG loss from Transmitter to Feed, (IL) = 0.79 dEm

Total Feed iInput Power in dB (P3) = P2—Loss = 26.99 dBm

Total Feed Input Power in Watts (P) = 10"°"" = 500 W

Antenna Isotropic Gain (G) = 46.5 dBi

Antenna Gain Converted to Power Ratio (Ges) = 10* = 44,668

Antenna Nomina! Efficiency (N) = 0.60



Far Field (Rf) = 0.6(1%) = 92 M

                                  Ges(P)
Far Field Power Density (Wf) =                    ——x 0.1 = 21.0 mwicm*
                                  Ar(Rf)

Near Field (Rn) = 14)7 = 38 M

                                  16N(P)JO,I
Near Field Power Density (Wn) = ]F>                       = 47.2 mwiom*
                                     [ #(12")


Transistion Region (RHL= Win = 47 2 e

                                            [2p|
main Keflector Region Power Density (Wm) = | —— 0 i =40.0 mwicm*
                                            1007 ;



                                                       T p1
Power Density between Main Reflector and Ground (Wq) = | :— }0.1 = 20.0 mw/icm*
                                                          0|




Far Field Off Axis (WF) = Wf(C.O1) = 0.21 mwicm*

Near Field Off Axis {WN) = Wn(0.01) = 0.472 mw/om*



Document Created: 2014-02-06 11:31:07
Document Modified: 2014-02-06 11:31:07

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