Attachment Exhibit A

This document pretains to SES-STA-20130809-00708 for Special Temporal Authority on a Satellite Earth Station filing.

IBFS_SESSTA2013080900708_1006908

                                                                           Lockheed Martin Corporation
                                                          Carpentersville, New Jersey Earth Station STA
                                                                                            August 2013
                                                                                            Attachment
                                                                                             Page 1 of 5


                                                     Description

         Lockheed Martin Corporation (“Lockheed Martin”) requests special temporary authority
(“STA”) to operate its Carpentersville, New Jersey Ku-band fixed earth station (see File No.
SES-LIC-20081103-01443, as amended) to provide telemetry, tracking and control (“TT&C”)
functions during the post-launch and transfer orbit phases of operation for the Eutelsat 25B
satellite.1 Eutelsat 25B, a satellite jointly licensed by France and Qatar and destined for the 25.5º
E.L. orbital location, is currently scheduled for launch on August 29, 2013 from the European
spaceport at Kourou, French Guiana.2 Accordingly, Lockheed Martin would likely need to begin
test transmissions in preparation for the launch on or about August 22, 2013.3

        Lockheed Martin specifically seeks authority to transmit telecommand signals on the
14.250 GHz and 14.4998 GHz frequencies for in transit communications and on the 14.0005
GHz and 14.0010 GHz frequencies for on-station operations, and to receive telemetry signals
from the satellite on the 11.1998 GHz and 11.6986 GHz frequencies. Lockheed Martin is
requesting the duration of this STA to be a total of 30 days from August 22, 2013, 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 for Eutelsat 25B within 10
days after the satellite is launched.

        The transmit frequencies that Lockheed Martin seeks to use for the Eutelsat 25B TT&C
launch and early operations support were part of Lockheed Martin’s license for Call Sign
E920702 and are specified in its current application for the Ku-band antenna in File No. SES-
LIC-20081130-01443 (under Call Sign E7541). Lockheed Martin’s proposed transmissions on
both transmit frequencies will use the emission designators for telecommand that are proposed in
the pending license application, or will use carriers that do not exceed the highest e.i.r.p., e.i.r.p.
density, and bandwidth prescribed in the application for the telecommand carriers. When no
commands are being sent, a CW carrier that is within the emission envelope proposed in
Lockheed Martin’s application, as amended, would be present. See File No. SES-AMD-
20081219-01664, at Schedule B. The information in the Schedule B portion of Lockheed
Martin’s pending application in File No. SES-LIC-20081130-01443, as amended, is hereby
incorporated by reference.

1
 The pending application in File No. SES-LIC-20081103-01443, under Call Sign E7541, was filed on a provisional
basis to replace Lockheed Martin’s inadvertently non-renewed license for a 14.2 meter Ku-band antenna at the
Carpentersville, NJ site under Call Sign E920702. Lockheed Martin’s petition to reinstate the license for Call Sign
E920702, as well as the “replacement” application it filed in the alternative under File No. SES-LIC-20081103-
01443 and Call Sign E7541, are pending.
2
    See, e.g., “SSL Delivers Satellite for Eutelsat, Es’hailSat,” Space News, Aug, 5, 2013.
3
  The test transmissions that would begin on or about August 22nd 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
                                                  Carpentersville, New Jersey Earth Station STA
                                                                                    August 2013
                                                                                    Attachment
                                                                                     Page 2 of 5


        Both of the frequencies on which satellite telemetry transmissions from Eutelsat 25B will
be received under the STA requested here are also included as receive frequencies in Lockheed
Martin’s Ku-band authorization under Call Sign E920702 and application under Call Sign
E7541. All of Lockheed Martin’s proposed TT&C operations in support of the Eutelsat 25B
launch will be on a strictly non-harmful interference, non-protected basis.

         Lockheed Martin believes that the limited operations it proposes in support of the launch
of Eutelsat 25B satellite – operations Lockheed Martin and the satellite operator will coordinate
in advance with any and all potentially affected entities that operate communications systems in
compliance with the Table of Frequency Allocations during the limited period of use – are
required in the public interest. Eutelsat 25B will allow expanded service and enhanced coverage
across the Middle East, North Africa and Central Asia as a follow on to Eutelsat 25C, which is
currently operated at 25.5° E.L. Lockheed Martin’s earth station will be part of a global network
of control facilities that will be used to position the satellite as it progresses from transfer orbit to
its final location. 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 Eutelsat 25B satellite is controlled while over North
America; Lockheed Martin’s earth station thus will serve a vital function.

        Lockheed Martin designates Michael Usarzewicz to be the contact person that will be
available whenever transmission to, or reception from, Eutelsat 25B is to occur through the
subject earth station. Mr. Usarzewicz can be reached at the following cell phone number: (609)-
865-2658 and/or station number: (908) 859-4050.

        The antenna to be used for this STA is already built. It is the same antenna that was
authorized under Call Sign E920270 and that is now the subject of the pending reinstatement
request described in Note 1 above, and has been used on an STA-basis to support other satellite
launches. See, e.g., Request of Lockheed Martin Corp. for STA to operate Carpentersville, NJ
earth station in support of launch of Amazonas-3, File No. SES-STA-20130122-00078 (granted
Feb. 4, 2013); Request of Lockheed Martin Corp. for STA to operate Carpentersville, NJ earth
station in support of launch of SES-4, File No. SES-STA-20111209-01447 (granted Dec. 14,
2011); Request of Lockheed Martin Corp. for STA to operate Carpentersville, NJ earth station in
support of launch of JCSAT-12, File No. SES-STA-20090615-00734 (granted July 20, 2009).
For this reason, Lockheed Martin does not provide a new analysis of non-ionizing radiation for
the antenna, or any of the detailed transmission/reception parameters for the signals. Instead,
Lockheed Martin incorporates by reference the radiation hazard study and Schedule B
information that were included with the November 2008 modification application in File No.
SES-LIC-20081103-01443, as amended.

        In sum, Lockheed Martin requests authority to operate its Carpentersville, NJ Ku-band
earth station antenna to provide critical TT&C services during the launch and early operations
phase of the Eutelsat 25B satellite, for a term of 30 days commencing August 22, 2013.


                                                            Lockheed Martin Corporation
                                           Carpentersville, New Jersey Earth Station STA
                                                                             August 2013
                                                                             Attachment
                                                                              Page 3 of 5


    Operating Parameters for Proposed Carpentersville, NJ Ku-Band TT&C LEOp STA



                      Parameter                                Performance
Orbit-Raising Operations and Contingency
Operations (Telemetry)
Antenna coverage                             +126° to -94° from +Z and +66° to -34° from –Z
Antenna polarization                         RHCP
Antenna configuration                        Four antennas
                                               Two +Z elements (11.2 GHz and 11.7 GHz)
                                               Two –Z elements (11.2 GHz and 11.7 GHz)
On-Station Normal Operations (Telemetry)
Antenna coverage                             Regional
Antenna polarization                         Linear, X-Polarization
Antenna configuration                        Global horn, off pointed towards Fucino
Orbit-Raising Operations and Contingency
Operations (Command)
Antenna coverage                             +126° to -94° from +Z and +66° to -34° from –Z
Antenna polarization                         LHCP
Antenna configuration                        Four antennas
                                               Two +Z elements (14.250 and 14.4998 GHz)
                                               Two -Z elements (14.250 and 14.4998 GHz)
On-Station Normal Operations (Command)
Antenna coverage                             Regional
Antenna polarization                         Linear, X-polarization
Antenna configuration                        Global horn, off pointed towards Fucino
Telemetry
Frequency                                    11.1998 GHz
                                             11.6986 GHz

Frequency stability                          ±1 ppm, 24 hour
                                             ±50 kHz, over life
Short-term phase stability                   10 Hz, -35 dBc/Hz
                                             100 Hz, -55 dBc/Hz
                                             1 kHz, -63 dBc/Hz
                                             100 kHz, -105 dBc/Hz


                                                   Lockheed Martin Corporation
                                  Carpentersville, New Jersey Earth Station STA
                                                                    August 2013
                                                                    Attachment
                                                                     Page 4 of 5




                      Parameter                       Performance
Telemetry (Cont’d)
Frequency stability                 ±1 ppm, 24-hour
                                    ±50 kHz, over life
Short-term phase stability          10 Hz, -35 dBc/Hz
                                    100 Hz, -55 dBc/Hz
                                    1 kHz, -63 dBc/Hz
                                    100 kHz, -105 dBc/Hz
EIRP variation                      0.2 dB p-p, any 2 minutes
EIRP
  Transfer orbit                    > 7 dBW
  Synchronous orbit                 > 15 dBW towards EOC
Modulation                          Phase modulation telemetry and/or ranging
  Telemetry
      PC1                           PCM/NRZ-L/BPSK 16 kbps on 128 kHz subcarrier
  Ranging                           Between 15 kHz and 50 kHz
Coding                              Viterbi, rate ½, 32,000 symbols/sec
Phase deviation                     Automatic gain controlled as follows:
  Ranging subcarrier                1.15 ±10% radian
  Ranging + Telemetry               1.15 ±10% radian
  TLM to RNG mod index ratio        2:1 (1.028 : 0.514 radian)
Command
Frequency                           14.250 and 14.4998 GHz (FM)
                                    14.0005 and 14.0010 GHz (PM) on-station
Uplink TCR Sites                    Nominal
                                       Rambouillet – France
                                       Sintra – Portugal
                                       Dubna – Russia
                                       Fucino – Italy
                                       Makarios – Cyprus
                                       Canical – Madeira
                                    West Beam
                                       Rambouillet – France
                                       Fucino – Italy
Flux density (min)
   Orbit Raising                    -89.5 dBW/m2
   Contingency                      -89.5 dBW/m2
   On-Station – Nominal             -113.0 dBW/m2
   On-Station – West                -102.0 dBW/m2
   No Damage                        -50 dBW/m2


                                                     Lockheed Martin Corporation
                                    Carpentersville, New Jersey Earth Station STA
                                                                      August 2013
                                                                      Attachment
                                                                       Page 5 of 5




                   Parameter                              Performance
Command (Cont’d)
Carrier modulation – FM
  Type                                Frequency Modulation (FM)
  Deviation                           ±400 kHz
Carrier modulation – PM
  Type                                Phase Modulation (PM)
  Modulation Index                    1 radian
  Bit rate                            1000 bps
Baseband encoding                     Non-Return to Zero-Level (NRZ-L)
  Data modulation                     Binary Phase-Shift Keyed (BPSK) on 16-kHz
                                      subcarrier, coherent
Ranging
Baseband                              Between 15 kHz and 50 kHz
Modulation
  Uplink                              Same as Command
  Downlink                            Same as Telemetry
End-to-end ranging delay accuracy     50 ns



Document Created: 2013-08-09 19:05:49
Document Modified: 2013-08-09 19:05:49

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