Attachment Order&Auth

Order&Auth

ORDER submitted by FCC

Order and Authorization, released November 20, 2007

2007-11-20

This document pretains to SES-LIC-20051028-01494 for License on a Satellite Earth Station filing.

IBFS_SESLIC2005102801494_606468

                                Federal Communications Commission                            DA 07- 4674


                                           Before the
                                Federal Communications Commission
                                      Washington, D.C. 20554


In the Matter of                                   )
                                                   )
ViaSat, Inc.                                       )         File No. SES-LIC-20051028-01494
                                                   )                  SES-AMD-20060314-00440
Application for Blanket Authority for Operation of )                  SES-AMD-20070309-00325
1,000 Technically Identical Ku-Band Aircraft       )         Call Sign : E050318
Earth Stations in the United States and Over       )
Territorial Waters                                 )


                                  ORDER AND AUTHORIZATION

     Adopted: November 19, 2007                                  Released: November 20, 2007

By the Chief, International Bureau and the Chief, Office of Engineering and Technology:

I.        INTRODUCTION

         1. With this order, we grant ViaSat, Inc. blanket authority for domestic operation of up to 1,000
technically identical transmit/receive earth stations aboard commercial aircraft. These earth stations will
provide Aeronautical Mobile Satellite Service (“AMSS”), using the standard Ku-band frequency ranges
14.0-14.5 GHz (Earth-to-space) and 11.7-12.2 GHz (space-to-Earth), to link with leased transponders
aboard the AMC-6 satellite operating at the 72º West Longitude orbital location. The ViaSat aircraft
earth stations will provide two-way broadband communications for passengers and aircrew members
aboard commercial airliners and private business jets, with access to email, the Internet, and corporate
virtual networks. Implementation of the ViaSat AMSS system pursuant to this authorization will enhance
competition in an important sector of the mobile telecommunications market in the United States.

II.       BACKGROUND

          A.       Preceding Developments Pertaining to AMSS Operation with Ku-Band FSS
                   Satellites

        2. In license orders issued in 2001, the International Bureau (“Bureau”) and the Office of
Engineering and Technology (“OET”) granted applications by The Boeing Company for authority to
provide AMSS in the 11.7-12.2 GHz and 14.0-14.5 GHz bands. At that time there was no allocation for
mobile-satellite service in those bands.1

        3. The 2003 World Radiocommunication Conference (WRC-03) added a worldwide secondary
Earth-to-space AMSS allocation in the 14.0-14.5 GHz band. At the same time, the International
Telecommunication Union’s Radiocommunication Sector adopted ITU-R M.1643, which sets forth



1
  Boeing Company Application for Blanket Authority to Operate Up to Eight Hundred Technically Identical
Transmit and Receive Mobile Earth Stations Aboard Aircraft in the 14.0-14.5 GHz and 11.7-12.2 GHz Frequency
Bands, Order and Authorization, 16 FCC Rcd 5864 (Int’l Bur. and OET, 2001) (“Boeing 12 GHz License Order”);
Order and Authorization, 16 FCC Rcd 22645 (Int’l Bur. and OET, 2001) (“Boeing 14 GHz License Order”).


                                     Federal Communications Commission                                DA 07-4674


detailed recommendations pertaining to operation of AMSS aircraft terminals in the 14 GHz band,2
including recommended interference-avoidance requirements that are essentially identical to conditions
previously imposed in the Boeing 14 GHz License Order.

        4. In November 2003 the Commission accordingly amended the U.S. Table of Frequency
Allocations to add a secondary Earth-to-space AMSS allocation in the 14.0-14.5 GHz band.3 Further, in a
Notice of Proposed Rulemaking released in February 2005 (“Ku-Band AMSS NPRM”), the Commission
proposed to amend the Table of Allocations to recognize AMSS operations in the 11.7-12.2 GHz band
and to establish rules prescribing licensing procedures and operational requirements for Ku-Band AMSS
operation.4 At present, however, there are no Commission service rules for licensing or operation of
AMSS in the 14.0-14.5 GHz band, and there is no domestic allocation for AMSS in the 11.7-12.2 GHz
band.

          5. In April 2005, the Bureau granted another operator, ARINC, a blanket license for operation
of AMSS terminals in the standard Ku Band for communication via leased transponders on an existing
satellite.5

           B.       ViaSat’s Application

         6. ViaSat filed its application on October 28, 2005. The application was found acceptable for
filing in a public notice issued in February 2006.6 No petitions or comments were filed in opposition to
the application.

        7. ViaSat’s planned AMSS system, which the applicant refers to by the tradename “Arclight,” is
designed to provide two-way broadband data communications via satellite radio links between aircraft
earth stations (“AES’s” or “AES terminals”) and a Ground Earth Station (“GES”) and Network
Operations Center (“NOC”). ViaSat proposes to use a previously-licensed GES located in Carlsbad,
California for this purpose, which ViaSat currently operates to support ARINC’s “SkyLink” AMSS
system. The Arclight AMSS NOC would be co-located with the GES.

       8. Arclight AES terminals, which have been certified by the Federal Aviation Administration,7
are comprised of three major sub-assemblies: an Airborne Integrated Transceiver Router (AITR), an
Antenna Control Unit (ACU) and a Tail-Mount Antenna Subsystem (TMASS). The AITR performs

2
  Rec. ITU-R M.1643, Technical and operational requirements for aircraft Earth stations of aeronautical mobile-
satellite service including those using fixed-satellite service network transponders in the band 14-14.5 GHz (Earth-
to-space) (2003).
3
  Amendment of Parts 2, 25, and 87 of the Commission’s Rules to Implement Decisions from the World
Radiocommunication Conferences Concerning Frequency Bands Between 28 MHz and 36 GHz and to Otherwise
Update the Rules in this Frequency Range, Report and Order, ET Docket No. 02-305, 18 FCC Rcd 23426 at ¶76
(2003). The amendment deleted a proviso that had limited the scope of the Mobile Satellite Services allocation in
the band in question by specifically excluding AMSS.
4
 Service Rules and Procedures to Govern the Use of Aeronautical Mobile Satellite Service Earth Stations in
Frequency Bands Allocated to the Fixed Satellite Service, Notice of Proposed Rulemaking, IB Docket No. 05-20, 20
FCC Rcd 2906 (2005).
5
  Application for Blanket Authority for Operation of up to One Thousand Technically Identical Ku-Band
Transmit/Receive Airborne Mobile Stations Aboard Aircraft Operating in the United States and Adjacent Waters,
Order and Authorization, 20 FCC Rcd 7553 (2005) (“ARINC AMSS License Order “).
6
    Report No. SES-00790, Satellite Radio Applications Accepted for Filing (Feb. 1, 2006).
7
  ViaSat Arclight AMSS Application, SES-LIC-20051028-01494, as amended by SES-AMD-20060314-00440
(“Arclight AMSS Application”), Exhibit 2 at § 2.2.1.

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                                      Federal Communications Commission                            DA 07-4674


multiple functions, which include packet routing at the local area network interface, IP data encapsulation
and recovery, downlink demodulation and decoding, uplink encoding and burst modulation,
implementation of power and frequency control algorithms, network communications with the NOC, and
control of the TMASS via the ACU. The main component of the TMASS is a steerable 0.2921 meter
(11.5 inch) parabolic reflector antenna, which can rotate in 3 axes and can receive in the 11.7-12.2 GHz
band while simultaneously transmitting in the 14.0-14.5 GHz band. The ACU uses data received from
the aircraft inertial navigation system to continuously control the AES antenna so that it points at the
target satellite as the aircraft executes flight maneuvers, with total root mean square pointing error of less
than 0.1° in normal operation. Any aircraft maneuver or navigational failure that prevents the antenna
from properly pointing to the target satellite will disrupt the received signal, with resultant shut down of
the AES transmitter within one second by on-board fault management controls designed to stop
transmission in the event of AES hardware failure or out-of-tolerance operation.8

        9. To establish a connection, an Arclight AES must initiate a login sequence after processing a
periodically-transmitted configuration message from the NOC via the assigned satellite transponder.
After processing the configuration message, the AES transmits a login burst lasting approximately 16
milliseconds at a low power level. If no response is received from the NOC, the AES transmits
successive login bursts at 10-second intervals, incrementally increasing power in 1-decibel steps up to a
preconfigured maximum. If no response is received after attempting login at the maximum power level,
the AES continues login attempts in a different frequency channel, starting at the lowest power level
again.9 Arclight AES terminals that are logged in transmit data in bursts at random time intervals, using a
Code Division Multiple Access “Aloha” contention access protocol and Direct Sequence Spread
Spectrum modulation with forward error control.10 The power of the data transmissions from a logged-in
AES terminal is dynamically controlled by the NOC, using a closed-loop algorithm that takes into
account the Eb/No ratio (energy per bit divided by noise density) of data transmissions received by the
GES and the aircraft’s location in relation to the gain/noise-temperature contour of the satellite antenna.11
The NOC also controls AES transmitter duty cycles and data-transmission rates, which can vary from 32
kbps to 512 kbps, and corrects frequency errors in AES transmissions.12

III.       DISCUSSION

           A.       Prevention of Interference in the 14.0-14.5 GHz Band

                    1.       Off-Axis equivalent isotropically radiated power (e.i.r.p.) Density

         10. An earth station antenna’s off-axis radiation, radiation in directions other than along the
antenna’s boresight, can interfere with a satellite adjacent to the earth station’s target satellite. In the
interest of minimizing such interference, Recommendation ITU-R M.1643 states that an AMSS system
that uses the 14.0-14.5 GHz band for AES uplink transmission should be operated in such a manner that
the aggregate off-axis e.i.r.p. density produced by simultaneously transmitting AES terminals in the
network do not exceed “the levels that have been published and coordinated for the specific and/or typical
earth station(s) pertaining to FSS networks ….”13

8
    Arclight AMSS Application, Exhibit 2 at §§ 2.2.1, 2.2.1.1, 2.2.1.2, and 2.2.1.3
9
    Arclight AMSS Application, Exhibit 2 at § 2.4.2.1
10
     Arclight AMSS Application, Exhibit 2 at §§ 3.1.2.2 and 3.2.1.
11
  Arclight AMSS Application, Exhibit 2 at § 2.4.4. ViaSat adds that these parameters will be used to estimate the
on-axis equivalent isotropically radiated power (e.i.r.p.) of AES data transmissions. Id.
12
     Arclight AMSS Application, Exhibit 2 at §§ 2.4.4, 2.4.5, and 2.4.6.
13
     Rec. ITU-R M.1643, Annex 1, Part A, ¶1.

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                                    Federal Communications Commission                                  DA 07-4674


          11. Although not directly applicable to AESs, the Commission’s rules for Fixed-Satellite Service
(FSS) earth stations provide guidance as to the technical criteria for evaluating AESs’ off-axis e.i.r.p.
density. Under the Commission’s rules, authority for operation of a single FSS earth station to provide
digital services in the 14.0-14.5 GHz uplink band can be routinely granted without coordination if the
station’s antenna equivalent diameter is 1.2 meters or more and the spectral density of the input power to
the antenna will not exceed -14 dBW/4kHz.14 The minimum antenna-diameter criterion effectively limits
eligibility for routine licensing to applications specifying antennas with gain patterns consistent with the
off-axis gain limits set forth in Section 25.209 of the Commission’s rules.15 A fixed earth station with an
antenna too small to meet the off-axis gain limits in Section 25.209 can be licensed pursuant to criteria
prescribed in Section 25.220(c).16 Paragraph (1) of Section 25.220(c) provides that authority for such a
non-conforming earth station may be granted if the applicant proposes to limit the maximum power
density of the signal input into the earth station’s antenna to a level determined by reducing the maximum
permissible input power density for a routinely-licensed station by the number of decibels that the non-
compliant antenna exceeds the applicable gain limits in Section 25.209.17 Alternatively, Section
25.220(c), Paragraph (2), provides that authority for operation of a non-conforming Ku-band earth station
that does not meet the input-power limit prescribed in Paragraph (1) may be granted if, inter alia, the
applicant files a statement from the operator of the target satellite certifying that it has coordinated the
proposed operation of the non-conforming earth station with the operators of all adjacent GSO satellites
within six degrees of separation.18

        12. In combination, the off-axis gain limits in Section 25.209 and the input power-density limit of
-14 dBW/4kHz specified in Section 25.212(c) effectively define the following maximum levels of
permissible off-axis e.i.r.p. density toward the geostationary-satellite-orbit arc from a single routinely-
licensed FSS earth station transmitting digitally modulated signals in the 14.0-14.5 GHz band:19
                   Angle off-axis            Maximum e.i.r.p. density in any 4 kHz band
                                        20
                   1.0º ≤ Theta ≤ 7.0º               15 -25log10Theta dBW
                   7.0° < Theta ≤ 9.2°               -6 dBW
                   9.2° < Theta ≤ 48º                18 -25log10Theta dBW
                          Theta > 48º                -24 dBW

14
  47 CFR § 25.212(c). To be eligible for routine processing, an application for a digital Ku-band earth station must
also specify a maximum downlink e.i.r.p. density no greater than 10 dBW/4kHz. See 47 CFR § 25.134(g)(2) and
2000 Biennial Regulatory Review – Streamlining and Other Revisions of Part 25 of the Commission’s Rules
Governing the Licensing of, and Spectrum Usage By, Satellite Network Earth Stations and Space Stations, Sixth
Report and Order, Fifth Report and Order, IB Docket No. 00-248, 20 FCC Rcd 5666 (2005) at ¶99.
15
   The Commission has determined that gain at off-axis angles of 1.25 degrees or more in the geostationary-satellite
orbital plane from a Ku-band earth station with a 1.2-meter transmitting antenna will not exceed the levels specified
in Section 25.209(a), 47 CFR § 25.209(a). 2000 Biennial Regulatory Review – Streamlining and Other Revisions of
Part 25 of the Commission’s Rules Governing the Licensing of, and Spectrum Usage By, Satellite Network Earth
Stations and Space Stations, Sixth Report and Order and Third Further Notice of Proposed Rulemaking, IB Docket
No. 00-248, 20 FCC Rcd 5593 (2005) (“Sixth Report and Order and Third FNPRM”) at ¶11 and n.27. Also see 47
CFR § 25.209(g) (gain limits for routinely-licensed Ku-band antennas with diameters of 1.2 meters or more apply at
off-axis angles of 1.25 degrees or more).
16
     See 47 CFR §§ 25.209, 25.220(c).
17
     Id.
18
     47 CFR § 25.220(c).
19
     See 47 CFR §§ 25.209, 25.212(c).
20
   For Ku-band earth stations with antennas between 1.2 meters and 5 meters in diameter, the 15 - 25log10θ dBW
limit applies at angles above 1.25 degrees rather than at angles above 1.0 degree. See 47 CFR § 25.209(g).

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                                         Federal Communications Commission                           DA 07-4674


where Theta is the angle in degrees from the axis of the main lobe.21 The Commission has proposed to
adopt a rule that would require each AES terminal in a Ku-band AMSS system to comply with these off-
axis e.i.r.p. limits (which we will refer to hereafter as “the routine-licensing off-axis radiation
envelope”).22

         13. ViaSat acknowledges that the antenna it proposes to incorporate in the Arclight AES
terminals is incapable, due to its small diameter, of meeting the off-axis gain limits for routinely-licensed
FSS earth stations in Section 25.209.23 Taking into account the measured gain pattern of the Arclight
AES antenna,24 it can be determined by calculation that the off-axis e.i.r.p. density radiated from a single
Arclight AES terminal toward the geostationary orbital arc will not exceed the routine-licensing off-axis
radiation envelope, provided that the maximum power density of the antenna input is limited to -24.25
dBW/4kHz. This power-density level is 10.25 dB below the limit for routinely-licensed Ku-band FSS
earth stations transmitting digitally modulated signals. ViaSat indicates in the Arclight AMSS application
that the power density of the input into an Arclight AES antenna will not exceed -29.08 dBW/4kHz.25
Thus, it appears that the off-axis e.i.r.p. density toward the geostationary orbital arc generated by a single
Arclight AES terminal will always be well below the routine-licensing off-axis radiation envelope.

        14. As we have noted, however, ViaSat proposes to use access protocols that could allow
multiple AES terminals to transmit in the same frequency channel at the same time.26 When an applicant
requests blanket authority for Ku-band earth stations to operate in a network with an access protocol that
could allow such simultaneous co-frequency AES transmissions, it is necessary to take into account the
combined off-axis radiation from simultaneously operating terminals as well as the levels of off-axis
radiation that a single terminal can generate to determine the aggregate e.i.r.p. density of the AES
transmissions.27 ViaSat initially proposed to allow aggregate off-axis e.i.r.p. density toward the
geostationary arc from simultaneously-transmitting Arclight AES terminals to exceed the routine-
licensing envelope for brief time periods.28 By amendment filed on March 9, 2007, however, ViaSat
withdrew this proposal.29 Rather, ViaSat now proposes to keep aggregate off-axis e.i.r.p. density from
AES operation within the routine-licensing envelope all of the time. ViaSat asserts that the Arclight NOC
would keep aggregate off-axis radiation within the envelope by dynamically controlling the input power
of individual AES terminals, monitoring and controlling the number of AES terminals accessing the
network, and limiting the number of data bursts AES terminals may send when the average number of
simultaneous transmissions exceeds a threshold determined by statistical algorithms.30

            15. ViaSat has filed a copy of a coordination letter signed by SES Americom, the licensed

21
  Moreover, the Commission has adopted these limits in its rules pertaining to operation of Ku-band earth stations
on vessels. See 47 CFR § 25.222(a)(1).
22
     Ku-Band AMSS NPRM at ¶36.
23
     Arclight AMSS Application, Exhibit 2 at § 5.2.1.1.
24
  See Arclight AMSS Application, Exhibit 2 at § 3.1.2.2, and letter with attachments dated Jan. 23, 2006 to the FCC
Secretary from Elizabeth R. Park, Counsel to ViaSat.
25
   See Arclight AMSS Application, Exhibit 2 at § 3.2.2, specifying that the spectral density of the aggregate (two-
frequency) return links will be approximately 15 dB-PSD below the level required at the authorized bandwidth.
26
     See ¶ 9, supra.
27
     See, e.g., 47 CFR § 25.222(a)(1).
28
     Arclight AMSS Application, Exhibit 2 at § 1.1.2.
29
     SES-AMD-20070309-00325.
30
     Id. at § 5.2.1.2.

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                                     Federal Communications Commission                                 DA 07-4674


operator of the AMC-6 satellite. In the letter, SES states its understanding that ViaSat will operate the
Arclight AMSS system in such a way that aggregate off-axis e.i.r.p. from Arclight AES terminals will
“always [be] equal to or less than that of routinely authorized VSAT [Very Small Aperture Terminal]”
remote stations. In other words, the aggregate off-axis e.i.r.p. will always be within the routine-licensing
off-axis radiation envelope. Further, AES operations would be consistent with coordination agreements
between SES and operators of adjacent satellites.31 The off-axis radiation limits that ViaSat proposes are
acceptable to PanAmSat, the operator of the only co-frequency satellite within six degrees of the AMC-6
satellite. We conclude that it would serve the public interest to authorize Arclight operation within those
limits, subject to the conditions imposed in this order and any additional requirements imposed in the
pending Ku-Band AMSS rulemaking. In the event another co-frequency FSS satellite commences
operation at a location within six degrees of the target satellite, ViaSat shall confine aggregate off-axis
radiation to a level one dB below the routine-processing limits, pending coordination with the operator of
the new satellite.32 Both previous recipients of license authority for Ku-band AMSS operation voluntarily
proposed to keep off-axis radiation from single terminals within a one-dB margin below the routine-
processing limits and to keep aggregate off-axis radiation within that margin for all but a small fraction of
the time.33 In view of the fact that ViaSat is proposing to operate with random-access protocols that
would allow simultaneous operation by multiple terminals, we think it is reasonable to require ViaSat to
meet a similar restriction during any period of time when its AMSS operation has not been coordinated
with respect to an operational co-frequency satellite within six degrees of the target satellite. We believe
this requirement will minimize the possibility of unacceptable interference to other licensed operations.

                    2.        Related Requirements Based on ITU-R M.1643

        16. In addition to proposing off-axis e.i.r.p. limits for Ku-band AMSS systems, the Commission
proposed several other technical requirements in the Ku-Band AMSS NPRM based on recommendations
in ITU-R M.1643 to minimize risk of harmful interference with co-channel FSS systems. Specifically,
the Commission proposed to adopt the following requirements pertaining to operation of Ku-band AES
terminals: maintaining pointing accuracy within 0.2 degrees; use of tracking algorithms that are resistant
to capturing signals from adjacent satellites; immediate cessation of transmission upon detection of
unintended satellite tracking; operational control by an NOC located in the United States that can detect
AES malfunctions and send “enable transmission” and “disable transmission” commands to the AES
terminals; automatic cessation of AES transmission upon receipt of a parameter-change command
pending receipt of an enable-transmission signal from the NOC; and on-board fault detection with
automatic shutdown upon detection of a fault that could result in harmful interference.34 Based on review
of the subject application, we conclude that operation of the Arclight AMSS system would satisfy these
proposed requirements.

                    3.        Protection of Space Research Service and Radio Astronomy

        17. The 14.0-14.2 GHz band is domestically allocated for secondary-status Federal-government
operation in the Space Research Service (“SRS”).35 The National Aeronautics and Space Administration
31
   Letter dated April 19, 2006 “To Whom It May Concern” from Krish Jonnalagadda, Manager of Satellite
Marketing Development for SES Americom, Inc., and Daryl T. Hunter. P.E., Senior Systems Engineer for ViaSat,
Inc., endorsed by Mohammad Marashi, Vice President of Customer Support Engineering for PanAmSat
Corporation.
32
   ViaSat may be subject to a different set of operating requirements due to adoption of applicable rules or policies
in the Ku-band AMSS rulemaking.
33
     See ARINC AMSS License Order at ¶¶ 18, 24 and 32.
34
     Ku-Band AMSS NPRM at ¶¶ 41-44.
35
     See 47 C.F.R. § 2.106.

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                                    Federal Communications Commission                          DA 07-4674


(“NASA”) currently operates SRS Tracking and Data Relay Satellite System (“TDRSS”) stations in
White Sands, New Mexico, and Guam that receive signals from geostationary satellites in the 14.0-14.05
GHz segment of the SRS band. NASA plans to establish an additional 14 GHz TDRSS station near
Blossom Point, Maryland. ITU-R M.1643 recommends that Ku-band AMSS systems be coordinated with
SRS operation by limiting AES emission levels, or terminating AES operation, in the vicinity of SRS
earth stations.36 The Commission has proposed to require Ku-band AMSS applicants to resolve concerns
regarding interference with SRS operation through coordination.37

        18. When it filed the Arclight AMSS blanket license application, ViaSat included a copy of a
coordination agreement signed in October 2005 by representatives of ViaSat and NASA.38 Under the
terms of the agreement, ViaSat must terminate transmissions from any Arclight AES that would exceed
defined interference thresholds when the AES is within line of sight of a TDRSS earth station, including
any such TDRSS station that commences operation in the future.

        19. The National Science Foundation (“NSF”), an independent Federal agency created by
Congress, supports radio-astronomy observation in the 14.47-14.5 GHz band at National Radio
Astronomy Observatories in New Mexico and West Virginia. The use of the band for radio-astronomy
observation at those sites is recognized in Footnote US203 to the U.S. Table of Allocations, which
requires steps to be taken to minimize interference with such operation from terrestrial radio transmitters.
The NSF also supports radio-astronomy observation in the same band at various other sites in the
continental United States, Hawaii, Puerto Rico, and the U.S. Virgin Islands.39 ITU-R M.1643
recommends that AES terminals cease transmission in the 14.47-14.5 GHz band and meet power flux
density (“PFD”) limits in the 14.0-14.47 GHz band when within line of sight of radio astronomy stations
observing in the 14.47-14.5 GHz band.40 The Commission has proposed to require Ku-band AMSS
applicants to resolve concerns regarding interference with such radio-astronomy observation stations
through coordination.41

        20. ViaSat states in its blanket license application that Arclight AES terminals will cease
transmission on frequencies above 14.44 GHz when within line of sight of a radio astronomy station
during periods of scheduled radio astronomy observation in the 14.47-14.5 GHz band. ViaSat also states
in the application that radiation in the 14.0-14.47 GHz band from Arclight AES terminals within line of
sight of radio astronomy stations during such periods of observation will not exceed the power flux
density limits specified in ITU-R M.1643: –190 + 0.5 · θ dB(W/(m2 · 150 kHz)) for θ ≤ 10° and –185
dB(W/(m2 · 150 kHz)) for 10° < θ ≤ 90°, where θ is the angle of arrival of the radio frequency wave
above the horizontal.42 Further, ViaSat filed a copy of a coordination agreement with the NSF, executed
in April 2006, in which ViaSat agreed to meet specified limits on aggregate PFD in the 14.47-14.5 GHz




36
     Rec. ITU-R M.1643, Annex 1, Part D.
37
     Ku-Band AMSS NPRM at ¶¶ 23 and 28.
38
  Coordination Agreement Between the National Aeronautics and Space Administration and VIASAT, Incorporated
for Operation of the VIASAT Arclight AMSS Operation in the 14.0-14.5 GHz Band, executed on Oct. 26, 2005.
39
     47 C.F.R. § 2.106, Footnote US203.
40
     Rec. ITU-R M.1643, Annex 1, Part B.
41
     Ku-Band AMSS NPRM at ¶¶ 23 and 28.
42
  Arclight AMSS Application, Exhibit 2 at § 5.2.4, as amended. The proposed PFD limits are identical to a
pertinent recommendation in ITU-R M.1643.

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                                     Federal Communications Commission                           DA 07-4674


band at various listed radio astronomy sites during periods of observation in that band.43

       21. The authorization granted in this order is subject to conditions requiring compliance with the
coordination agreements with NASA and the NSF as well as any additional requirements that the
Commission adopts in the Ku-Band AMSS rulemaking proceeding with respect to protection of Federal-
government operations in the 14.0-14.5 GHz band.

                    4.      Protection of Terrestrial Radio Services

        22. ITU-R M.1643 recommends adoption of PFD limits on emissions from AES terminals in the
14.0-14.5 GHz band when they are within line of sight of any territory where fixed terrestrial networks
are in operation.44 The 14.2-14.4 GHz band is domestically allocated on a secondary basis for
grandfathered operation of land mobile stations licensed prior to March 2, 2005.45 The 14.4-14.5 GHz
band is allocated on a secondary basis for governmental fixed and mobile services.46

         23. ViaSat asserts in its blanket-license application that there are no terrestrial radio services
licensed for operation in North America in the 14.0-14.5 GHz band that would receive interference from
operation of Arclight AES terminals. According to ViaSat, it is highly unlikely that AES terminals that
transmit only when locked onto a geostationary target satellite would ever transmit in the direction of a
ground-based radio station within the latitudes of the continental United States. Nevertheless, ViaSat
states that Arclight AES terminals in aircraft at altitudes of 5,000 feet or higher will operate in compliance
with the recommended PFD limits specified in ITU-R M.1643 when their antennas are pointed at an angle
of 15 degrees above horizontal. According to ViaSat, this scenario is the worst case possible for Arclight
AES operations in continental-US airspace.47 Based on ViaSat’s representation, it appears that the PFD
from Arclight AES terminals will always be within the limits specified in M.1643. We do not authorize
Arclight AES operation with PFD in excess of those limits.

           B.       Downlink Transmission in the 11.7-12.2 GHz Band

        24. The 11.7-12.2 GHz band is domestically allocated on a primary basis for FSS downlink
transmission, including downlink transmission to earth stations on vessels,48 and is allocated on a
secondary basis for operation of grandfathered terrestrial radio stations.49 The Commission has proposed
to add an allocation for AMSS downlinks in the 11.7-12.2 GHz band,50 but there is no AMSS allocation
in the band at the present time. Hence, ViaSat requests a waiver to permit operations in the 11.7-12.2


43
  Coordination Agreement Between the National Science Foundation and ViaSat, Inc. for Operation of the ViaSat
Arclight AMSS and Radio Astronomy Sites Jointly Sharing the 14.0-14.5 GHz Band, filed as attachment to letter
dated Apr. 12, 2006 to the FCC Secretary from Elizabeth R. Park, Counsel to ViaSat.
44
  Specifically, ITU-R M.1643 recommends adoption of PFD limits of -132 + 0.5·θ dBW(W/(m2·MHz)) for θ ≤ 40°
and -112 dBW(W/(m2·MHz)) for 40° < θ ≤ 90º, where theta is the angle of arrival of the AES emissions in degrees
above the horizontal. See Rec. ITU-R M.1643, Annex 1, Part B.
45
     47 CFR § 2.106, Footnote NG184.
46
     47 CFR § 2.106.
47
     Arclight AMSS Application, Technical Description § 5.2.2.
48
  47 CFR § 2.106, Footnotes NG145 and NG183, and Procedures to Govern the Use of Satellite Earth Stations on
Board Vessels in the 5925-6425 MHz/3700-4200 MHz Bands and 14.0-14.5 GHz/11.7-12.2 GHz Bands (Report and
Order), IB Docket No. 02-10, FCC 04-286, 20 FCC Rcd 674 (2005) at ¶79.
49
     47 CFR § 2.106, Footnote NG184.
50
     Ku-Band AMSS NPRM at ¶15

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                                     Federal Communications Commission                                 DA 07-4674


GHz band on a non-interference, non-protected basis.51

          25. Section 25.134(g)(2) of the Commission’s rules specifies a limit of 10 dBW/4kHz on the
e.i.r.p. density of digital satellite transmissions in the 11.7-12.2 GHz band for routinely-licensed VSAT
systems.52 An applicant proposing to operate with satellite carrier e.i.r.p. density above 10 dBW/4kHz
must file, in its application, a statement from the target satellite operator attesting that it has coordinated
such proposed operation with the operators of other geostationary satellites within 6 degrees of orbital
separation.53 ViaSat indicates in its application that the e.i.r.p. density of Arclight AMSS downlink
transmissions in the 11.7-12.2 GHz band will not exceed 9.82 dBW/4kHz.54 Moreover, SES, the target
satellite operator, and PanAmSat, which operates the only co-frequency satellite within six longitudinal
degrees, have certified that the proposed downlink operation would be consistent with the terms of the
coordination agreements reached by the affected operators.55

        26. The Commission has previously granted authority to Boeing and ARINC for use of the 11.7-
12.2 GHz band for AMSS downlink transmission from existing FSS satellites, based on a showing that
the 10 dBW/4kHz limit would not be exceeded or proof of consent by adjacent satellite operators.56
Consistent with these precedents, we conclude that a waiver is warranted to allow ViaSat to use the 11.7-
12.2 GHz band for AMSS downlinks on a non-interference, non-protected basis.


IV.        CONCLUSION

        27. We find, pursuant to Section 309 of the Communications Act, 47 U.S.C. § 309, that grant of
blanket authority for ViaSat to operate its proposed Arclight AMSS system, as conditioned herein, will
serve the public interest, convenience, and necessity.


V.         ORDERING CLAUSES

         28. Accordingly, IT IS ORDERED that ViaSat, Inc.’s application, File Nos. SES-LIC-20051028-
01494, as amended by File Nos.SES-AMD-20060314-00440 and SES-AMD-20070309-00325, IS
GRANTED to the extent indicated herein, and ViaSat, Inc. IS AUTHORIZED to operate up to 1,000
technically-identical transmit/receive mobile earth stations aboard aircraft operating with the AMC-6
satellite at orbital location 72° W.L., in the 11.7-12.2 GHz and 14.0-14.5 GHz frequency bands in the

51
     See 47 CFR § 2.102(a).
52
     47 CFR § 25.134(g)(2).
53
  47 CFR § 25.220(e)(1)(ii). See 2000 Biennial Regulatory Review – Streamlining and Other Revisions of Part 25
of the Commission’s Rules Governing the Licensing of, and Spectrum Usage By, Satellite Network Earth Stations
and Space Stations, Fifth Report and Order in Docket 00-248, 20 FCC Rcd 5666 (2005) at ¶¶ 93-95 (concluding
that authority should be routinely granted for digital downlink transmission in the 11.7-12.2 GHz band with e.i.r.p.
density up to 10 dBW/4kHz without requiring coordination).
54
     Arclight AMSS Application, Technical Description § 3.3.2.
55
   Letter dated April 19, 2006 “To Whom It May Concern” from Krish Jonnalagadda, Manager of Satellite
Marketing Development for SES Americom, Inc., and Daryl T. Huner. P.E., Senior Systems Engineer for ViaSat,
Inc., endorsed by Mohammad Marashi, Vice President of Customer Support Engineering for PanAmSat
Corporation.
56
   Boeing 12 GHz License Order at ¶10 (granting blanket license conditioned on submission of proof that operators
of adjacent satellites had no objection to proposed operation with peak downlink e.i.r.p. density in excess of the 10
dBW/4KHz routine-licensing limit); ARINC AMSS License Order at ¶54 (noting that proposed maximum downlink
e.i.r.p. density was well below 10 dBW/4kHz).

                                                          9


                                Federal Communications Commission                           DA 07-4674


continental United States and over its territorial waters, consistent with the specifications in the
application and in compliance with the Commission’s rules, except insofar as waived herein, and subject
to the following conditions.
   a) The Arclight AMSS system must operate in compliance with any rule requirements subsequently
      adopted by the Commission.
   b) The Arclight AMSS system must accept interference from lawful operation of any station in the
      11.7-12.2 GHz band in accordance with the U.S. Table of Frequency Allocations (47 C.F.R. §
      2.106) and shall immediately terminate operation upon notification that such operation is causing
      harmful interference, not permitted under the terms of a pertinent coordination agreement, with
      lawful operation of any radio system in the 11.7-12.2 GHz band in conformance with the U.S.
      Table of Frequency Allocations.
   c) Arclight AMSS operation shall immediately terminate upon notification that such operation is
      causing harmful interference, not permitted under the terms of pertinent coordination agreements,
      with (1) lawful operation of any radio system in the 14.0-14.5 GHz band authorized on a primary
      basis in conformance with the U.S. Table of Frequency Allocations or authorized on a secondary
      basis prior to the effective date of this order, or (2) operation of any TDRSS earth station in the
      band 14-14.2 GHz, or (3) radio astronomy observations in the 14.47-14.5 GHz band.
   d) The Arclight AMSS licensee shall maintain a point of contact for discussing interference
      concerns with other licensees and U.S. Government agencies and shall submit a letter to be
      included in its license file with the name and telephone number of the contact prior to
      commencing operation.
   e) Arclight AES terminals must employ a tracking algorithm that is resistant to capturing and
      tracking adjacent satellite signals, and each AES terminal must be capable of inhibiting its own
      transmission in the event it detects unintended satellite tracking.
   f) Arclight AES terminals must be monitored and controlled by a ground-based network control and
      monitoring center. Each Arclight AES terminal must be able to receive “enable transmission”
      and disable transmission” commands from the network control center and must cease
      transmission immediately after receiving any “parameter change” command until it receives an
      “enable transmission” command from the network control center. The network control center
      will monitor operation of each Arclight AES terminal to determine if it is malfunctioning, and
      each Arclight AES terminal will self-monitor and automatically cease transmission on detecting
      an operational fault that could cause harmful interference to the fixed satellite service network.
   g) Arclight AMSS operation in the 11.7-12.2 GHz band shall be in accordance with the space station
      authorization for the AMC-6 satellite.
   h) The Arclight AMSS system shall not be used to provide air traffic control communications.
   i)   The Arclight AMSS system shall operate in compliance with any limits established by the
        International Telecommunication Union (ITU) to protect other services allocated internationally.
   j)   Operation pursuant to this authorization shall conform to the requirements of ViaSat’s
        coordination agreements with NASA and NSF as well as its coordination agreement with SES
        Americom and PanAmSat.
   k) The licensee shall notify the Commission of the date when commercial operation of the Arclight
      AMSS system commences. 12 months after commencing commercial operation, the licensee
      shall file a report on the system’s aggregate off-axis radiation performance since the
      commencement of commercial operation, based on the most recent available data and taking into
      account all relevant variables, including the following:
            mispointing of AES antennas due to bias, latency, tracking error, and misalignment between
            transmit and receive apertures;
                                                10


                                    Federal Communications Commission                            DA 07-4674


                variation in AES antenna gain patterns due to manufacturing tolerances, aging,
                environmental effects, scan angle variation, element phase error, amplitude error, and failure
                rate;
                variations in AES transmit e.i.r.p. due to measurement error, control error, and latency
                affecting closed-loop power control.57
       l)   In the event that another co-frequency FSS satellite commences operation at a location within six
            degrees of the target satellite, ViaSat must reduce aggregate off-axis radiation from Arclight AES
            terminals to levels one dB below the routine-processing envelope, pending demonstration of
            coordination with the operator of the new satellite.

        29. IT IS FURTHER ORDERED that Section 2.102 of the Commission’s rules IS WAIVED with
respect to operation of the Arclight AMSS network in the 11.7-12.2 GHz downlink band consistent with
the terms of this authorization.

         30. ViaSat may decline this authorization as conditioned within 30 days from the date of release
of this Order and Authorization. Failure to respond within that period will constitute formal acceptance
of the authorization as conditioned.

        31. This Order and Authorization is issued on delegated authority pursuant to Sections 0.241 and
0.261 of the Commission’s rules, 47 C.F.R. §§ 0.241 and 0.261, and is effective upon release.


                                               FEDERAL COMMUNICATIONS COMMISION


                                               Helen Domenici
                                               Chief, International Bureau



                                               Julius Knapp
                                               Chief, Office of Engineering and Technology




57
     See Rec. ITU-R M.1643, Annex 1, Part A.

                                                         11



Document Created: 2007-11-20 13:01:31
Document Modified: 2007-11-20 13:01:31

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