Attachment 20161220090004-683.p

20161220090004-683.p

DECISION submitted by FCC-IB

Grant

2016-12-20

This document pretains to SES-STA-20161123-00910 for Special Temporal Authority on a Satellite Earth Station filing.

IBFS_SESSTA2016112300910_1162201

                                             E7541      SES-STA-20161 123-00910   1B2016002546
                                             Lockheed Martin Corporation




                            APPLICATION FOR EARTH STATION SPECIAL TEMPORARY AUTHORITY


APPLICANT INFORMATIONEnter a description of this application to identify it on the main menu:
Carpentersville LEOP TT&C STA for JCSat 15 - Dec 2016 (30-Day STA)
 1. Applicant

           Name:        Lockheed Martin Corporation          Phone Number:                       703-413-5747
           DBA Name:                                         Fax Number:                         703-413-5908
           Street:      2121 Crystal Drive                   E-Mail:                             ryan.n.terry1rnco.cor
                        Suite 100
           City:        Arlington                            State:                              VA
           Country:     USA                                  Zipcode:                            22202
           Attention:   Ryan N. Terry


Applicant: Lockheed Martin Corporation
Call Sign: E7541
File No.:  SES-STA-20161 123-00910
Special Temporary Authority (STA)


Lockheed Martin Corporation is granted STA for 30 days to operate its earth station Call Sign
E7541 in Carpentersville, New Jersey to provide telemetry, tracking and control ("TT&C")
functions during the post-launch and transfer orbit phases (LEOP) for JCSAT- 15 at 1100 W.L.
on frequencies 13750.5 MHz and 13754.5 MHz (Earth-to-space) and 12201.0 MHz and 12203.0
MHz (space-to-Earth). Operations are authorized under the following conditions:


1.     Operations will not exceed the operational power levels and parameters requested and
coordinated.
2. All operations under this grant of STA shall be on an unprotected and non- harmful
interference basis. Lockheed Martin Corporation shall not cause harmful interference to, and
shall not claim protection from interference caused to it by, any other lawfully operating radio
communication system.
3. In the event of any harmful interference Lockheed Martin Corporation shall cease operations
immediately upon notification of such interference, and shall immediately inform the
Commission, in writing, of such an event.
4. The LEOP operations must be coordinated with all operators of satellites that use the same
frequency bands and are in the LEOP path. All operators of satellites in that path will be
provided with an emergency phone number where the licensee can be reached in the event that
harmful interference occurs. Currently the 24x7 contact information for the JCSAT-15 satellite
LEOP mission is as follows: Cell Phone: (609) 865-2658 and/or station number (908) 859-4050.
Request to speak with Mr. Usarzewicz.
5. All operations must comply with the EIRP limitations established in 47 C.F.R. § 2.106
Footnote US 356 and US 357.
6. Grant of this STA is without prejudice to any determination that the Commission may make
regarding pending or future Lockheed Martin Corporation LLC applications.
7. Any action taken or expense incurred as a result of operations pursuant to this STA is solely
at Lockheed Martin Corporation LLC's risk.
This grant is issued pursuant to Section 0.26 1 of the Commissions rules on delegated authority,
47 C.F.R. § 0.261, and is effective upon release.                        "J./             s
                                                                   Fie #    ;S7-O/(, f/. &o


2. Contact

             Name:         Ryan N. Teny                         Phone Number:                        703-413-5747
             Company:      Lockheed Martin Corporation          Fax Number:                          703-413-5908
             Street:       2121 Crystal Drive                   E-Mail:                              ryan.n.terry@lmco.co
                           Suite 100
             City:         Washington                           State:                                DC
             Country:      USA                                  Zipcode:                             22202      -
             Attention:                                         Relationship:                         Same


(If your application is related to an application filed with the Commission, enter either the file number or the TB Submissi
application. Please enter only one.)
 3. Reference File Number SESLIC20081 10301443 or Submission ID
   4a. Is a fee submitted with this application?
• If Yes, complete and attach FCC Form 159.        If No, indicate reason for fee exemption (se e 47 C.F.R.Section 1.1114).
    Governmental Entity
                             Q Noncommercial educational licensee
o Other(please explain):
4b. Fee Classification    CGX - Fixed Satellite Transmit/Receive Earth Station
5. Type Request


    Use Prior to Grant                                Change Station Location


9. State   NJ                                                               10. Longitude
                                                                            (dd mm ss.s h)    75   11     27.8   W
11. Please supply any need attachments.
Attachment 1: STA                                 Attachment 2:                                         Attachment 3:


12. Description.   (If the complete description does not appear in this box, please go to the end of the form to view it in its
    Lockheed Martin Corporation hereby requests Special Temporary Authority beginn
    17, 2016, to operate its Carpentersville, New Jersey fixed earth station (Call
    to provide telemetry, tracking and control (TT&C) functions during the post-la
    early orbit phases (LEOP) of operation for the JCSAT-l5 satellite.




13. By checking Yes, the undersigned certifies that neither applicant nor any other party to the application is
subject to a denial of Federal benefits that includes FCC benefits pursuant to Section 5301 of the Anti-Drug Act
of 1988, 21 U.S.C. Section 862, because of a conviction for possession or distribution of a controlled substance.
See 47 CFR 1.2002(b) for the meaning of "party to the application" for these purposes.


14. Name of Person Signing                                                  15. Title of Person Signing
  Jennifer A. Warren                                                          Vice President, Technology Policy & Regulati
           WILLFUL FALSE STATEMENTS MADE ON THIS FORM ARE PUNISHABLE BY FINE AND / OR IMPR
                  (U.S. Code, Title 18, Section 1001), AND/OR REVOCATION OF ANY STATION AUTHORIZATIO
                   (U.S. Code, Title 47, Section 3 12(a)(1)), AND/OR FORFEITURE (U.S. Code, Title 47, Section 50


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                                                                      Lockheed Martin Corporation
                                                                 Call Sign E7541 Earth Station STA
                                                                                       Attachment
                                                                                        Page 1 of 2




                    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 E745 1)
to provide telemetry, tracking and control ("TT&C") functions during the post-launch and early
orbit phases ("LEOP") of operation for the JCSAT-1 5 satellite.

        JCSAT-15 is destined for in-service operation at 110.00 E.L., and is currently scheduled
for launch on December 20, 2016, aboard an Ariane-5ECA from the European Spaceport in
Kourou, French Guiana.

       Accordingly, Lockheed Martin requests to begin test transmissions on December 17,
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- 15 satellite is launched.

        1.      Requested STA Operations

        Lockheed Martin specifically seeks authority to transmit telecommand signals at the
center frequencies 13750.5 MHz and 13754.5 MHz for in transit telecommand communications
(Earth-to-space), and to receive telemetry signals from the satellite (space-to-Earth) at the center
frequencies 12201.0 MHz and 12203.0 MHz.

        The proposed TT&C operations in support of the JCSAT-l5 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, E1RP 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.



  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 E7541 Earth Station STA
                                                                                      Attachment
                                                                                       Page 2 of 2




        Lockheed Martin designates Michael Usarzewicz to be the contact person that will be
available whenever transmission to, or reception from, JCSAT- 15 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- 15 satellite serve the public interest. Lockheed Martin understands that the
JCSAT-1 5 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- 15 satellite is controlled while over North America en route to its final geo stationary
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-15 satellite, for a term of 30 days, commencing December 17, 2016.


                                 TC&R Subsystem Performance

                    Parameter                                      Performance
Orbit-Raising Operations and Contingency
Operations (Telemetry)
Antenna coverage                                 l300   to +900 from +Z and   700   to +30° from -z
Antenna polarization                            Linear Horizontal Polarization (HP)
Antenna configuration                           Four antennas
                                                   Two +Z elements
                                                   Two -Z elements
On-Station Normal Operations (Telemetry)
Antenna coverage                                Ku-band Japan beam
Antenna polarization                            Right Hand Circular Polarization (RHCP)
Antenna configuration                           Ku-band Japan transmit antenna
Orbit-Raising Operations and Contingency
Operations (Command)
Antenna coverage                                -130° to +90° from +Z and -70° to +30° from -Z
Antenna polarization                            Left-Hand Circular Polarization (LHCP)
Antenna configuration                           Four antennas
                                                   Two +Z elements
                                                   Two -Z elements
On-Station Normal Operations (Command)
Antenna coverage                                Ku-band Japan Regional Coverage
Antenna polarization                            Linear Vertical Polarization (VP)
Antenna configuration                           Ku-band Command Horn
Telemetry
Frequency                                       12.201 GHz RHCP
                                                12.203 GHz RHCP
EIRP
  Wide-angle antenna                            3 dBW (mm at EU C), 10 dBW (max)
    Ku-Band Japan Communications antenna (On-   22 dBW
station)
Modulation                                      Phase modulation telemetry and/or ranging
Telemetry
   Subcarrier frequencies
       Physical Channel 1                       128 kHz


                       Parameter                                  Performance
      Physical Channel 2                       320 kHz (Back up only)
   Output data
      Normal/Dwell telemetry                   128 kHz (Normal + Dwell)
   Data rate                                   BPSK on 128-kHz subcarrier
   Data modulation                             16,000 bps
                                               Bi-phase L
Ranging                                        27.777-kHz 7 tones ESA ranging subcarrier
Modulation index
   One subcarrier                              1.0 ±0.1 radian
   Two subcarriers                             0.7 ±0.1 radian
   Three subcarriers                           0.58 ±0.1 radian
Phase Noise                                    4 deg rms
Command
Frequency
                                               13.7505 GHz VP (On-Station)
                                               13.7545 GHz and 13.7505 GHz LHCP (Orbit-
                                               raising/Contingency)
Flux density (mm)
   Transfer orbit and contingency on-station   ?-90 dBW/m2
   Normal on-station                           2 IO5dBW/m2
   No Response                                 -120 dBW/m
   No damage                                   -50 dBW/m
Modulation
   Type                                        FM
   Deviation                                   ±400 kHz
   Bit rate                                    1,000 bps
Baseband encoding                              Non-return to Zero-Level (NRZ-L) Binary Phase-
                                               Shift Keyed (BPSK)
   Data modulation                             Binary Phase-Shift Keyed (BPSK) on 1 6-kHz
                                               subcarrier, coherent
Ranging
Baseband                                       Rangingtones 7-tone-27.7 kHz ESA-like (on-
                                               station) or Intelsat tone burst ranging scheme
Flux density                                   > -86 dBW/m2 (Contingency)
                                               > -101 dBW/m2 (Normal on-station)
Modulation


                   Parameter                      Performance
  Uplink                       FM, ±400-kHz carrier deviation
  Downlink                     PM, 1.0 E0.1 radian, 0.7 ±0.1 radian, or 0.58 ±0.1
                               radian
Ranging accuracy               ± 15 m, On-station
                               ±30 m, Transfer Orbit


              Antenna Gain

The Tx antenna gain at 13.75 GHz = 63.3 dBi


                       SUPPLEMENT: Transmit Power

The proposed operations will be limited to a maximum transmit power of 84 dBW.


              SUPPLEMENT: EIRP Density

       The proposed operations will be limited to a
maximum EIRP density of 24 dBW/4kHz for the subject carrier.


                     Supplemental Information for SES-STA-20161123-00910

        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, mi sec- NAD 83)           75 ° 11 27.8 "W
  Latitude (deg, mm, see- 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

Command:

13.7545 GHz LHCP
13.7505 GHz LHCP

Telemetry:

12.201 GHzRHCP
12.203 GHz RHCP



Document Created: 0000-00-00 00:00:00
Document Modified: 0000-00-00 00:00:00

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