Attachment FCC 96-377 Analysis

This document pretains to SES-AMD-20171115-01256 for Amended Filing on a Satellite Earth Station filing.

IBFS_SESAMD2017111501256_1303785

                                        The Boeing Company
                                            Herndon, VA

                              GD Vertex 3.8 Meter Earth Station
1. Background
This Exhibit is presented to demonstrate the extent to which The Boeing Company satellite
earth station in Herndon, VA is in compliance with the Federal Communications
Commission (“FCC”) Report and Order 96-377. The potential for interference from the earth
station to U.S. Navy Shipboard radiolocation operations (“Radar”) and the National
Aeronautics and Space Administration (“NASA”) space research activities in the 13.75-14
GHz band is addressed in this exhibit. The parameters for the earth station are:


Coordinates (NAD83):                                      38o 57’ 32.0‘N, 77o 22’32.0‘W
Satellite Location for Earth Station:                     Telstar 12V, at the 15° W.L.
Frequency Band:                                           13.75-14.0 GHz
Polarizations:                                            Linear
Emissions:                                                8M00G7W
Modulation:
Maximum Aggregate Uplink EIRP:                            65.04 dBW
Transmit Antenna Characteristics:
Antenna Size:                                             3.8M
Antenna Type/Model:                                       GD Vertex RSI
Gain:                                                     53.0 dBi
RF Power into Antenna Flange:                             12.04 dBW
Minimum Elevation Angle:                                  10.9 @ 264.2
                                                          12.7 @ 108.2

Side Lobe Antenna Gain                                    FCC Reference Pattern
Because the above uplink spectrum is shared with the Federal Government, coordination in
this band requires resolution data pertaining to the potential for interference between the earth
station and the U.S. Navy Department systems. Potential interference from the earth station
could impact the U.S. Navy Radiolocation and Radio Navigation systems, noted in the FCC
Report and Order 96-377 dated September 1996.


   Summary of Coordination Issues:
   a.) Potential for Impact to Government Radiolocation (Shipboard Radar)
   b.) Potential for Impact to NASA Tracking and Data Relay Satellite Systems (“TDRSS”)

   2. Potential for Interference to Government Radiolocation (Shipboard Radar)
   Radiolocation operations (“Radar”) may occur anywhere in the 13.4-10.0 GHz band aboard
   ocean-going U.S. Navy ships. FCC order 96-377 allocates the upper 250MHz of the 600 MHz
   band to the Fixed Satellite Service (“FSS”) on a co-primary basis with the radiolocation
   operations and provides for an interference protection level of -167 dBW/m2/4kHz.
       1.   Clear Sky EIRP:                                           65.04 dBW
       2.   Carrier Bandwidth:                                        8000KHz
       3.   PD at the Antenna input:`                                 -21dBW/4kHz
       4.   Transmit Antenna Gain:                                    53 dBi
       5.   Antenna Gain to Horizon:                                  3.1 dBi
       6.   Antenna Elevation Angles:                                 10.9 @ 264.2o azimuth
                                                                      12.7 @ 108.2o azimuth
The earth station will radiate toward the ocean according to its off-axis side-lobe performance. A
conservative analysis, using FCC standard reference pattern, results in an off-axis antenna gain of
11.52 towards the nearest shoreline.
The signal density at the shoreline was calculated using the ITU-R P.452 propagation model.
Using this model, Boeing calculates a propagation loss of 165.5 dB, resulting in a PFD of -
187.84 dBW/m2/4kHz, which is 20 dB below the protection criteria of -167 dbW/m2/4kHZ (see
Annex A for analysis)..
   3. Potential for Impact to NASA’s Tracking and Data Relay Satellite System
The geographic location of the Boeing earth station in Herndon, VA is within the 390 km radius
coordination contour surrounding NASA’s Blossom Point, MD ground station complex. However,
the Herndon ground station has proposed to operate in the 13-90-14.0 GHz band. Therefore the
TDRSS space-to-earth link will not be impacted by the Boeing earth station in Herndon, VA.
   4. Coordination Result Summary and Conclusions
The results of the analysis and calculations set forth in this exhibit indicate that the earth station
operations at the Herndon, VA facility and the U.S. Navy RADAR or NASA TDRSS space-earth
and space-space operations should be compatible. No harmful interference to U.S. Navy RADAR
or NASA TDRSS from the Herndon, VA site earth station should occur.


                                                Annex A
                                        ITU-R P.452 analysis


Introduction
To calculate propagation loss for this showing, the ITU-R P.452-16 propagation model was used.
ITU-R P.452 is a widely used terrain model for modeling path prediction for two stations on the
surface of the earth. ITU-R P.452 is a good model to use for this scenario since it specializes in
calculating path loss for coastal areas
ITU-R P.452 analysis
Figure 1 provides the path profile for this section. The transmitting station is at the Herndon site
and the receiving station was selected at 37.27N, 75.67W. A time percentage selection was also
made of 0.01%.


                                        Figure 1: Path Profile

                                Path Profile
 160.00

 140.00

 120.00

 100.00

  80.00

  60.00

  40.00

  20.00

   0.00
      0.0000    50.0000   100.0000   150.0000   200.0000   250.0000   300.0000


X-Axis Distance (Km)
Y-Axis Elevation (m)



Document Created: 2017-11-15 05:30:39
Document Modified: 2017-11-15 05:30:39

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