Attachment FAA Clarification

FAA Clarification

LETTER submitted by Telenor Satellite, Inc.

FAA Clarification

2006-09-07

This document pretains to SES-MFS-20060725-01253 for Modification w/ Foreign Satellite (earth station) on a Satellite Earth Station filing.

IBFS_SESMFS2006072501253_526370

                                                                                                                   ) telenor
                                                                                                                         Keith H. Fagan
                                                                                                                         Senior Counsel




                                                                   September 7, 2006

      Marlene H. Dortch
      Secretary
      Federal Communications Commission
      Washington, D.C. 20554

                  To:         International Bureau
                              Systems Analysis Branch

                  Re:         SES—MFS—20060725—01253 (Call Sign E980136)

      Dear Ms. Dortch:

              At the request of the International Bureau, Telenor Satellite, Inc. wishes to clarify that the
      navigational transponder on Inmarsat 3F4 has its own antenna, which provides global coverage.
      This is explained in more detail in the Technical Description that was attached as an exhibit to
      the above—referenced application. Following is an excerpt from that Technical Description.
                 The navigation payload has its own single feed and reflector mounted on the earth—
                 pointing nadir panel providing global coverage. The navigation transponder is
                 implemented in two parts, a C—L link and a C—C link. These two links are generated from
                 the same uplink feeder link signal. The transponder receives navigational positioning
                 signals in the C—band at 6.4 GHz for transmission to users in the L—band at 1.5 GHz
                 together with a simultaneous transmission of the same signal in the C—band at 3.6 GHz.
                 The purpose of the C—band downlink is to allow the feeder link earth station to make
                 adjustments to the timing of the uplink feeder link signal. (Page 12)

              Any further questions with respect to the above—referenced application should be directed
      to the undersigned.


                                                                                 Respectfully submitted,

                                                                                    0 AA s M           R   7~§7C"—"


                                                                                 Ketth H. Fagan



  _                 _                                                                                                          —          — \‘

Telenor Satellite Services Holdings, Inc.   Address:                     Telephone:        E—mail:                                           |
                                            1101 Wootton Parkway         +1 301 838 7860   keith.fagan@telenor—usa.com                       \
                                            10th Floor                   Fax:              Web site:                                         |
                                            Rockville, MD 20852 USA      +1 301 838 7752   telenor.com/satellite                             I



Document Created: 2019-05-26 01:04:31
Document Modified: 2019-05-26 01:04:31

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