Technical Description Overview

0379-EX-ST-2003 Text Documents

Hughes Network Systems, Inc.

2003-10-08ELS_63245

                                  ATTACHMENT 1


                    TECHNICAL DESCRIPTION OF THE
               Ka-BAND SATELLITE SIMULATION TEST RANGE


A. PURPOSE

  Hughes Network Systems, Inc. (“HNS”) is launching the first SPACEWAY satellite
  during the first quarter of 2004 to provide commercial service to North America during
  the middle of 2004. SPACEWAY is a next generation satellite system which will operate
  in Ka-band spectrum globally allocated for the Fixed-Satellite Services. The
  SPACEWAY system will employ new technologies for on-board digital processing,
  packet switching and spot-beams that do not yet exist on any US commercial satellite that
  is currently available.

  HNS is developing a Ka-band Satellite Simulation test environment comprised of a
  radiated far-field test environment for testing SPACEWAY satellite user terminals
  (“STs”) using a transmitter/receiver that will simulate a SPACEWAY satellite on the
  ground (“Satellite Simulator Terminal”). Because HNS’s Ka band satellites have not yet
  been launched, this test environment is necessary to allow HNS to test the user terminals
  designed for this unique satellite system. Such testing is designed to ensure that the
  technical and operational system performance specifications and features of the STs are
  met. The following sections of this Attachment describe this test facility.

B. TEST FACILITY DESCRIPTION

  The test range is located at the Headquarters of Hughes Network Systems at 11717
  Exploration Lane, Germantown, Maryland. The test range (see Figure 1) is 656 feet long
  and will support the testing of the STs that are 66cm, 74cm and 98cm in equivalent
  diameter. These transmit/receive terminals will be located at 39o10’45.9” North Latitude
  and 77o14’49.1” West Longitude on the ground near the D building of HNS
  Headquarters.

  The test STs will transmit signals in the frequency band from 29.5 GHz to 30.0 GHz
  utilizing two types of transmitters (2.1 Watts and 3.5 Watts) and three different antennas:
  98 cm circular, 74 cm elliptical, and 66 cm elliptical. The maximum output power of
  these transmitters will be limited to 0.5 Watts. The emission designators of these signals
  will be 650KG7W, 2M61G7W and 20M9G7W using QPSK modulation. This
  application requests authority to use 40 2.1 Watt transmitters and 40 3.5 Watt
  transmitters, however, only one ST will transmit using a single carrier at any given time.

  The SPACEWAY Satellite Simulator Terminal employs a 74cm antenna connected to a
  satellite payload emulator. This terminal will be located at 39o10’43.4” North Latitude
  and 77o14’41.4” West Longitude on the roof of the D building. This Satellite Simulator


  Terminal will transmit a broadband QPSK modulated carrier with an emission designator
  of 500MG7W centered at 19.95 GHz. The transmit input power to the 74cm Satellite
  Simulator Terminal antenna will be limited to a maximum of 10 nanowatts.

  HNS would like to start the testing on this Satellite Simulation test range on November 1,
  2003 and continue over a period of twenty-four months so that the performance of the
  various user terminal types can be thoroughly tested.

  HNS is applying for an STA simultaneously with this application so that it may operate
  these test facilities as soon as possible.

C. INTERFERENCE TO OTHER SERVICES

  The test facility proposed by this application is not likely to cause interference to any
  other licensed services or systems. The particular Ka-band frequencies HNS requests are
  not allocated to terrestrial systems, so the earth station transmissions will not cause
  interference to any licensed terrestrial systems. The only commercial or government
  satellite system currently operating over the US in this portion of the Ka-band, of which
  HNS is aware is ACTS; however, all transmissions in this proposed test range will
  operate at very low elevation angles (i.e. close to two degrees. See Figure 1). Operation
  at this low elevation will ensure that interference is not received by any satellite systems
  that may be operating in this portion of the Ka-band.


D. RF RADIATION COMPLIANCE

  The operation of these transmit/receive terminals at the HNS satellite simulation test
  facility will be in full compliance with the Commission’s radio frequency (RF) exposure
  guidelines, pursuant to Section 1.1307(b)(1) through (b)(3) of the Commission’s rules.
  Attachment 2 provides the radiation calculations for the three types of terminals to be
  tested in this facility. These analyses show that the power density levels will never
  exceed the Maximum Permissible Exposure (MPE) limit of 1 milliwatt per centimeter
  squared for the persons in General Population/Uncontrolled environment as specified in
  the Office of Engineering and Technology (OET) Bulletin No. 65 except in the region
  between the feed and the reflector. To ensure compliance with the FCC MPE limit, the
  terminal transmitter will be turned off whenever test personnel are required to work
  within this potentially hazardous area, and the terminals will be secured from access by
  the general public.


                                                 Figure 1

                                                                        D Roof - Satellite Simulator
                                                                                  Terminal
                      Test STs                                                    491' ASL
              98 cm circular or 74 cm
               elliptical (98x 56cm)
                                                                        39° 10' 43.4“ North Latitude
           or 66cm elliptical (74 x 59 cm)                             77° 14' 41.4“ West Longitude
                   fixedantenna
                                                                              Azimuth = 302°
                                              Uplink 29.5-30GHz
                                                                           Elevation Angle = +2°
                                             Down link19.7-20.2GHz                    74cmelliptical
                                                                                      (0.98 x 0.56 m)
                                                                                      fixedantenna


         A-Shed - ST
          499' ASL
 39° 10' 45.9“ North Latitude                                                     D Building
77° 14' 49.1" West Longitude
       Azimuth = 125°
    Elevation angle = -2°

                                    Distance Between A Shed and D Roof = 655.8'



                                  Satellite Simulation Farfield Range



Document Created: 2003-10-08 14:12:36
Document Modified: 2003-10-08 14:12:36

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