Attachment STA

This document pretains to SES-STA-20160713-00647 for Special Temporal Authority on a Satellite Earth Station filing.

IBFS_SESSTA2016071300647_1143087

                                                                     Lockheed Martin Corporation
                                                                Call Sign E7451 Earth Station STA
                                                                                      Attachment
                                                                                       Page 1 of 4




                    Description of Operations and Public Interest Statement

         Pursuant to 47 CFR 25.120 of the Commission’s Rules, Lockheed Martin Corporation
(“Lockheed Martin”) hereby requests Special Temporary Authority (“STA”) for a period of
thirty (30) days to operate its Carpentersville, New Jersey fixed earth station (Call Sign E7451)
to provide telemetry, tracking and control (“TT&C”) functions during the post-launch and early
orbit phases (“LEOP”) of operation for the JCSAT-16 satellite.

        JCSAT-16 is destined for in-service operation at 150.0° E.L., and is currently scheduled
for launch by mid-August aboard a Falcon 9 launch vehicle from Cape Canaveral, Florida.

        Accordingly, Lockheed Martin requests to begin test transmissions on August 10, 2016 in
preparation for the launch.1 Further, Lockheed Martin is requesting that the duration of this STA
be a total of thirty (30) days to cover any slippage in the anticipated dates of the various phases
of operation; it nonetheless expects that all Carpentersville operations in support of the launch
will be completed within fourteen (14) days after the JCSAT-16 satellite is launched.

        1.      Requested STA Operations

        Lockheed Martin specifically seeks authority to transmit telecommand signals at the
center frequencies 13751.0 MHz and 13753.0 MHz for in transit telecommand communications
(Earth-to-space), and to receive telemetry signals from the satellite (space-to-Earth) at the center
frequencies 12201.5 MHz and 12203.5 MHz.

        The proposed TT&C operations in support of the JCSAT-16 launch will be on a strictly
non-harmful interference, non-protected basis. Lockheed Martin’s proposed transmissions will
use total input power and emissions for Ku-band telecommand that will fall below the highest
input power, EIRP, EIRP density, and bandwidth prescribed for the telecommand carriers in its
above-referenced FCC license. When no commands are being sent, a CW carrier that is within
the emission of the licensed operation would be present. However, in the case of an anomaly,
extraordinary measures, such as increasing power, may be necessary; if such measures are
required during this STA period, Lockheed Martin will notify the FCC within seven (7) business
days that such measures were needed.

       Lockheed Martin incorporates by reference the radiation hazard study and Schedule B
information that were included with its most recent filings at the FCC.




1
  The proposed test transmissions would occur over a period of approximately two to three days. During
these tests, the earth station would not be communicating with any satellite; instead, the transmissions
will be made with the antenna at zenith to verify RF functionality.


                                                                   Lockheed Martin Corporation
                                                              Call Sign E7451 Earth Station STA
                                                                                    Attachment
                                                                                     Page 2 of 4




        Lockheed Martin designates Michael Usarzewicz to be the contact person that will be
available whenever transmission to, or reception from, JCSAT-16 is to occur through the subject
earth station. Mr. Usarzewicz can be reached at the following phone numbers:
        (609) 865-2658 (cellular)
        (908) 859-4050 (earth station desk)

       2. Grant of the Requested Authority Will Serve the Public Interest

        Lockheed Martin believes that the limited operations it proposes in support of the launch
of the JCSAT-16 satellite serve the public interest. Lockheed Martin understands that the
JCSAT-16 satellite has been licensed by the Japanese administration for the provision of
communications services to Japanese satellite operator SKY Perfect JSAT. Lockheed Martin’s
Carpentersville earth station will be part of a global network of control facilities that will be used
solely to position the satellite as it progresses from transfer orbit to its final location. No end
user service will be provided within the United States at any time. The safe and orderly use of
the entire geostationary orbital resource and protection of the hundreds of satellites licensed by
the U.S. and other countries that operate there depends in no small part on ensuring that the
JCSAT-16 satellite is controlled while over North America en route to its final geostationary
orbital position. In this regard, Lockheed Martin’s earth station thus will serve a vital function.


                                      *    *    *   *    *

       Lockheed Martin requests authority to operate its Carpentersville, NJ earth station
antenna to provide critical TT&C services during the launch and early operations phase of the
JCSAT-16 satellite, for a term of 30 days, commencing August 10, 2016.


                                                                        Lockheed Martin Corporation
                                                                   Call Sign E7451 Earth Station STA
                                                                                         Attachment
                                                                                          Page 3 of 4




         Operating Parameters for Proposed Carpentersville, NJ Ku-band TT&C LEOP STA

  SITE NAME (or identifier):                    Carpentersville, NJ – Call Sign E7541

  Antenna location
  Longitude (deg, min, sec- NAD 83)               75 ° 11 ' 27.8 " W
  Latitude (deg, min, sec- NAD 83)                40 ° 38 ' 39.1 " N
  Antenna Height:                                 19.2 m
  Ground Elevation (AMSL):                        85.7 m

  Antenna Characteristics (size & gain)

  Size                              14.2
  TX Gain                           63.5 dBi @ 14.0 GHz
  RX Gain                           62.9 dBi @ 12.0 GHz
  Antenna Model                     14.2 KFPA
  Antenna Manufacturer              TIW (GD SATCOM)

Maximum Power (at Flange)                500 W

     General
Satellite Name        Commercial name for the satellite                                    JCSat 16
Orbital Location      Longitude of the satellite in-service location                       150deg.E
IOT location          Longitude of the location where the IOT testing will be conducted    150deg.E

Mission Duration      Describe in months the amount of time the antenna is required for    .5 month
                      the mission
Expected launch       Planned satellite launch date                                        16-Aug-16
date
Operator              Name of the operator of the satellite                                   SSL
Manufacturer          Name of the manufacturer of the satellite                               SSL
  Telecommand
      Uplink
TC1 Center            Center frequency of TC1 in MHz                                       13753.00
Frequency
TC1 Bandwidth         TC1 carrier maximum occupied RF bandwidth in kHz                       1000
TC1 Start Frequency   Calculated start frequency for TC1 carrier                           13752.50
TC1 End Frequency     Calculated end frequency for TC1 carrier                             13753.50
TC1 Polarization      Polarization for TC1 carrier                                           LHCP
TC2 Center            Center frequency of TC2 in MHz                                       13751.00


                                                                        Lockheed Martin Corporation
                                                                   Call Sign E7451 Earth Station STA
                                                                                         Attachment
                                                                                          Page 4 of 4




Frequency
TC2 Bandwidth         TC2 carrier maximum occupied RF bandwidth in kHz                         1000
TC2 Start Frequency   Calculated start frequency for TC2 carrier                             13750.50
TC2 End Frequency     Calculated end frequency for TC2 carrier                               13751.50
TC2 Polarization      Polarization for TC2 carrier                                             LHCP
Data Rate             Data rate for command carriers                                          1 kbps
Modulation Type(s)    Type(s) of modulation for command carriers (i.e. FM, BPSK etc.)     1000bps, NRZ-
                                                                                            L/BPSK/FM
Emission              ITU standard code to represent bandwidth and modulation of           1M00F2DAN
Designator(s)         a carrier (i.e. 800KF8D). See Emission Designator tab for more
                      information
 Ranging Uplink
Bandwidth             Ranging carrier maximum occupied RF bandwidth in kHz                    1000
Modulation Type       Type of modulation (i.e. FM, QPSK, 16QAM, etc.)                        CW-FM
Emission              ITU standard code to represent bandwidth and modulation of            1M00F8XJN
Designator(s)         a carrier (i.e. 800KF8D). See Emission Designator tab for more
                      information
    Telemetry
    downlink
TM1 Center            Center frequency of TM1 in MHz                                         12201.50
Frequency
TM1 Bandwidth         TM1 carrier maximum occupied RF bandwidth in kHz                         1500
TM1 Start Frequency   Calculated start frequency for TM1 carrier                             12200.75
TM1 End Frequency     Calculated end frequency for TM1 carrier                               12202.25
TM1 Polarization      Polarization for TM1 carrier                                              HP
TM2 Center            Center frequency of TM2 in MHz                                         12203.50
Frequency
TM2 Bandwidth         TM2 carrier maximum occupied RF bandwidth in kHz                         1500
TM2 Start Frequency   Calculated start frequency for TM2 carrier                             12202.75
TM2 End Frequency     Calculated end frequency for TM2 carrier                               12204.25
TM2 Polarization      Polarization for TM2 carrier                                              HP
Data Rate             Data rate for command carriers                                          16 kbps
Modulation Type(s)    Type(s) of modulation (i.e. FM, BPSK,etc.)                        PM, BPSK PCM/NRZ-L
Emission              ITU standard code to represent bandwidth and modulation of           1M00G8DAN
Designator(s)         a carrier (i.e. 800KF8D). See Emission Designator tab for more
                      information



Document Created: 2016-07-13 11:54:49
Document Modified: 2016-07-13 11:54:49

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