Concept of Operations Description

0990-EX-ST-2016 Text Documents

L-3 Communications

2016-06-30ELS_178954

L-3 Communications, CS-W                                            STA File No.: 0990-EX-ST-2016
Special Temporary Authorization                                     STA Conf. No.: EL565737
Date: 06/30/2016                                                    License: TBD

ITAR Statement:
This technical data is controlled under the International Traffic in Arms Regulations (ITAR)
USML Category XI(d) and may not be exported to a Foreign Person, either in the U.S. or abroad,
without a license or exemption from the U.S. Department of State.

Distribution Statement:
Distribution authorized to the Department of Defense (DoD) and U.S. DoD contractors;
Administrative or Operational Use, March 1, 2014. Other requests for this document shall be
referred to DARPA, Security and Intelligence Directorate, 675 N. Randolph St., Arlington,
Virginia 22203-2114.

Application Background:

The purpose of this project is to ground and flight test with point-to-point data links for
application to mobile communications with hotspots for military applications. This application is
very similar to File No. EL745412; STA File No.: 0824-EX-ST-2016; License WJ9XYX. This
new application adds an airborne element to the test scenario.

Concept of Operations:

There will be up to 4 test stations operating up to 3 different simultaneous data links. The test
stations are both ground based and airborne based. The aircraft is a PA-31-350 Piper Navajo
Super Chieftain. Maximum altitude is 12.5kft or 3810m MSL with typical altitude being 10kft
or 3048m MSL. The three links are referred to as the Discovery Link, the E-band link, and the
Rover link.

Figure 1 illustrates the concept of operations for ground-to-ground-to-airborne testing where the
green arrow is the Discovery Link, the red arrow is the E-band link, and the black arrow is the
Rover link. Testing may include ground-to-ground tests, airborne-to-ground tests, or ground-to-
ground-to-airborne tests.

The 4 test stations and associated data links are defined below:

   •   Station #1 will operate a Discovery link and E-band link simultaneously and is ground
       based.

   •   Station #2 will operate a Discovery link and E-band link simultaneously and is ground
       based.

   •   Station #3 will operate a Discovery link, an E-band link, and a Rover-Vortex link
       simultaneously and is airborne based.


   •   Station #4 will operate a Rover-TNR link and is ground based. Station #4 may at times
       be co-located with Station #2.

Spectrum Requirements:

Discovery Link:
The discovery link will operate in the unlicensed 900 MHz ISM band (902.2464-927.8208
MHz). The radio is a commercial off the shelf product (MM2-EX family) made by Freewave
Inc. The radio uses a spread spectrum frequency hopping waveform. The radio is connected to
an omni antenna.

E-band Link:
The E-band link will operate in either the 71-76 GHz or 81-86 GHz frequency bands. The radio
is an L-3 custom product designed for these bands. Four data rates are included in the E-band
radio which uses S-OQPSK for the 2 higher data rates and DPSK for the 2 lower data rates. All
waveforms use 7/8 LDPC FEC with root raised cosine filtering α=0.33. The radio is connected
to an axially displaced ellipse directional tracking antenna with 39 dBi gain, RHCP polarization,
and 1.6° 3 dB beamwidth.

Rover Link:
The Rover link is comprised of two radios; an airborne L-3 Vortex transceiver (DD1494 J/F
12/09626) and a ground based L-3 Tactical Network ROVER (TNR) transceiver. The Rover-
Vortex link will operate in C-band (4.4-4.94 GHz) for the down link and the Rover-TNR link
will operate in S-band (2.2-2.29 GHz) for the uplink. The radios are both connected to omni
antennas. DD1494’s are available for both radios.


                                                                                               Station #3 Airborne
                                                                                               Discovery, E-band,
                                                                                                  Rover-Vortex
                                                                                                   Freewave MM2-EX 900 MHz
                                                                                                        1.5 W EIRP OMNI
                                                                                                      210KF1D or 220KF1D

                                                                                                     L3 CSW E-band 71/81
                                                                                                  P/N 1000391701/1000391702
                                                                                                       40.3 dBi Directional
                                                                                                     760MG1D, 75M9G1D,
                                                                                                      15M2G1D,1M52G1D

                                                                                                          L3 CSW Vortex
                                                                                                          P/N 60065293
                                                                                                        3.1 W EIRP OMNI
                                                                                                  C-band down link (4.4-4.94 GHz)
                                                                                                  2M28G1D, 4M55G1D, 9M10G1D




Station #1 Ground                     Station #2 Ground
Discovery, E-band                     Discovery, E-band
Freewave MM2-EX 900 MHz              Freewave MM2-EX 900 MHz
                                          1.5 W EIRP OMNI                      Station #4 Ground
     1.5 W EIRP OMNI
   210KF1D or 220KF1D                   210KF1D or 220KF1D                        Rover - TNR
                                                                               L3 CSW Rover – TNR
   L3 CSW E-band 71/81                                                             P/N 60116572
                                      L3 CSW E-band 71/81
P/N 1000391701/1000391702                                                       0.63 W EIRP OMNI
                                   P/N 1000391701/1000391702
     40.3 dBi Directional                                                   S-band up link (2.2-2.29 GHz)
                                        40.3 dBi Directional
   760MG1D, 75M9G1D,                                                       2M28G1D, 4M55G1D, 9M10G1D
                                      760MG1D, 75M9G1D,
    15M2G1D,1M52G1D
                                       15M2G1D,1M52G1D



                            Figure 1 Concept of Operations – Ground & Flight Test


Ground & Flight Testing Summary

Location of Ground Equipment:

The approximate locations of the ground stations are shown in Figure 2.

    Ground station #1, Discovery and E-band, approximate location:
    Lat: N 400 54’ 39.04”, Long: W 1110 50’ 37.35”, Alt 6357 feet (in the foothills above Bountiful, UT).
    Ground station #2, Discovery and E-band, approximate location:
    Lat: N 400 47’ 01.46”, Long: W 1110 57’ 07.65”, Alt 4269 feet (on the L-3 CSW campus).
    Ground Station #4, Tactical Network Rover, approximate location:
    Lat: N 400 28’ 45”, Long: W 1110 50’ 18.50”, Alt 6220 feet (in the foothills above Draper, UT).




                                Figure 2 Locations of Ground Test Equipment


Location of Airborne Equipment:

The approximate location of the aircraft flight profile is shown in Figure 3. Typical altitude is 10 kft MSL.
Approximate waypoints are listed below:

       WP1: (Lat: N 400 44’ 00”, Long: W 1110 53’ 00”)
       WP2: (Lat: N 400 27’ 00”, Long: W 1110 53’ 00”)
       WP3: (Lat: N 400 27’ 00”, Long: W 1110 47’39”)
       WP4: (Lat: N 400 44’ 00”, Long: W 1110 47’ 39”)

       Racetrack center at Lat: N 400 35’30”, Long: W 1110 50’10”)
       Approximately 20 miles north to south length
       Approximately 5 miles west to east width




                                 Figure 3 Location of Flight Test Equipment



Document Created: 2016-06-30 14:54:02
Document Modified: 2016-06-30 14:54:02

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