[Code of Federal Regulations]

[Title 47, Volume 2]

[Revised as of October 1, 2004]

From the U.S. Government Printing Office via GPO Access

[CITE: 47CFR25.138]



[Page 290-292]

 

                       TITLE 47--TELECOMMUNICATION

 

                    CHAPTER I--FEDERAL COMMUNICATIONS

                         COMMISSION (CONTINUED)

 

PART 25_SATELLITE COMMUNICATIONS--Table of Contents

 

                   Subpart B_Applications and Licenses

 

Sec. 25.138  Blanket Licensing provisions of GSO FSS Earth Stations in 



the 18.3-18.8 GHz (space-to-Earth), 19.7-20.2 GHz (space-to-Earth), 

28.35-28.6 GHz (Earth-to-space), and 29.25-30.0 GHz (Earth-to-space) bands.



    (a) All applications for a blanket earth station license in the GSO 

FSS in the 18.3-18.8 GHz, 19.7-20.2 GHz, 28.35-28.6 GHz, and 29.25-30.0 

GHz bands that meet the following requirements shall be routinely 

processed:

    (1) GSO FSS earth station antenna off-axis EIRP spectral density for 

co-polarized signals shall not exceed the following values, within 

3[deg] of the GSO arc, under clear sky conditions:









18.5-25log([thetas])-10log(N  dBW/40kHz...........  for 2.0[deg] <=

 ).                                                  [thetas] <= 7[deg]

-2.63-10log(N)..............  dBW/40kHz...........  for 7[deg] <=

                                                     [thetas] <=

                                                     9.23[deg]

21.5-25log([thetas])-10log(N  dBW/40kHz...........  for 9.23[deg] <=

 ).                                                  [thetas] <= 48[deg]

-10.5-10log(N)..............  dBW/40kHz...........  for 48[deg] <

                                                     [thetas] <=

                                                     180[deg]





Where:



[thetas] is the angle in degrees from the axis of the main lobe; for 

systems where more than one earth station is expected to transmit 

simultaneously in the same bandwidth, e.g., CDMA systems,

N is the likely maximum number of simultaneously transmitting co-

frequency earth stations in the receive beam of the satellite; N=1 for 

TDMA and FDMA systems.



    (2) GSO FSS earth station antenna off-axis EIRP spectral density for 

co-polarized signals shall not exceed the following values, for all 

directions other than within 3[deg] of the GSO 

arc, under clear sky conditions:









21.5-25log([thetas])-10log(N  dBW/40kHz...........  for 3.5[deg] <=

 ).                                                  [thetas] <= 7[deg]

0.37-10log(N)...............  dBW/40kHz...........  for 7[deg] <

                                                     [thetas] <=

                                                     9.23[deg]

24.5-25log([thetas])-10log(N  dBW/40kHz...........  for 9.23[deg] <

 ).                                                  [thetas] <= 48[deg]

-7.5-10log(N)...............  dBW/40kHz...........  for 48[deg] <

                                                     [thetas] <=

                                                     180[deg]







[[Page 291]]



Where:



[thetas]: is the angle in degrees from the axis of the main lobe; for 

systems where more than one earth station is expected to transmit 

simultaneously in the same bandwidth, e.g., CDMA systems.

N: is the likely maximum number of simultaneously transmitting co-

frequency earth stations in the receive beam of the satellite; N=1 for 

TDMA and FDMA systems.



    (3) The values given in paragraphs (a) (1) and (2) of this section 

may be exceeded by 3 dB, for values of [thetas] 10[deg], 

provided that the total angular range over which this occurs does not 

exceed 20[deg] when measured along both sides of the GSO arc.

    (4) GSO FSS earth station antenna off-axis EIRP spectral density for 

cross-polarized signals shall not exceed the following values, in all 

directions relative to the GSO arc, under clear sky conditions:









8.5-25log([thetas])-10log(N)  dBW/40kHz...........  for 2.0[deg] <=

                                                     [thetas] <= 7[deg]

12.63-10log(N)..............  dBW/40kHz...........  for 7[deg] <

                                                     [thetas] <=

                                                     9.23[deg]





Where:



[thetas]: is the angle in degrees from the axis of the main lobe; for 

systems where more than one earth station is expected to transmit 

simultaneously in the same bandwidth, e.g., CDMA systems.

N: is the likely maximum number of simultaneously transmitting co-

frequency earth stations in the receive beam of the satellite; N=1 for 

TDMA and FDMA systems.



    (5) For earth stations employing uplink power control, the values in 

paragraphs (a) (1), (2), and (4) of this section may be exceeded by up 

to 20 dB under conditions of uplink fading due to precipitation. The 

amount of such increase in excess of the actual amount of monitored 

excess attenuation over clear sky propagation conditions shall not 

exceed 1.5 dB or 15 % of the actual amount of monitored excess 

attenuation in dB, whichever is larger, with a confidence level of 90 

percent except over transient periods accounting for no more than 0.5% 

of the time during which the excess is no more than 4.0 dB.

    (6) Power flux-density (PFD) at the Earth's surface produced by 

emissions from a space station for all conditions, including clear sky, 

and for all methods of modulation shall not exceed a level of -118 dBW/

m\2\/MHz, in addition to the limits specified in Sec. 25.208 (d).

    (b) Each applicant for earth station license(s) that proposes levels 

in excess of those defined in paragraph (a) of this section shall submit 

link budget analyses of the operations proposed along with a detailed 

written explanation of how each uplink and each transmitted satellite 

carrier density figure is derived. Applicants shall also submit a 

narrative summary which must indicate whether there are margin 

shortfalls in any of the current baseline services as a result of the 

addition of the applicant's higher power service, and if so, how the 

applicant intends to resolve those margin short falls. Applicants shall 

certify that all potentially affected parties (i.e., those GSO FSS 

satellite networks that are 2, 4, and 6 degrees apart) acknowledge and 

do not object to the use of the applicant's higher power densities.

    (c) Licensees authorized pursuant to paragraph (b) of this section 

shall bear the burden of coordinating with any future applicants or 

licensees whose proposed compliant operations at 6 degrees or smaller 

orbital spacing, as defined by paragraph (a) of this section, is 

potentially or actually adversely affected by the operation of the non-

compliant licensee. If no good faith agreement can be reached, however, 

the non-compliant licensee shall reduce its earth station and space 

station power density levels to be compliant with those specified in 

paragraph (a) of this section.

    (d) The applicant shall provide for each earth station antenna type, 

a series of radiation patterns measured on a production antenna 

performed on a calibrated antenna range and, as a minimum, shall be made 

at the bottom, middle, and top frequencies of the 30 GHz band. The 

radiation patterns are:



[[Page 292]]



    (1) Co-polarized patterns for each of two orthogonal senses of 

polarizations in two orthogonal planes of the antenna.

    (i) In the azimuth plane, plus and minus 10 degrees and plus and 

minus 180 degrees.

    (ii) In the elevation plane, zero to 30 degrees.

    (2) Cross-polarization patterns in the E- and H-planes, plus and 

minus 10 degrees.

    (3) Main beam gain.

    (e) Protection of receive earth stations from adjacent satellite 

interference is based on either the antenna performance specified in 

Sec. 25.209 (a) and (b), or the actual receiving earth station antenna 

performance, if actual performance provides greater isolation from 

adjacent satellite interference. For purposes of insuring the correct 

level of protection, the applicant shall provide, for each earth station 

antenna type, the antenna performance plots for the 20 GHz band, 

including the format specified in paragraph (d) of this section.

    (f) The earth station licensee shall not transmit towards a GSO FSS 

satellite unless it has prior authorization from the satellite operator 

or a space segment vendor authorized by the satellite operator. The 

specific transmission shall be conducted in accordance with the 

operating protocol specified by the satellite operator. The holder of an 

FCC blanket license pursuant to this section shall be responsible for 

operation of any transceiver to receive GSO FSS service provided by that 

licensee or provided by another party with the blanket licensee's 

consent. Operators of GSO FSS systems shall not transmit communications 

to or from user transceivers in the United States unless such 

communications are authorized under a service contract with the holder 

of a pertinent FCC blanket license or under a service contract with 

another party with authority for such transceiver operation delegated by 

such a blanket licensee.

    (g) A licensee applying to renew its license must include on FCC 

Form 405 the number of constructed earth stations.



[65 FR 54169, Sept. 7, 2000, as amended at 66 FR 63515, Dec. 7, 2001; 68 

FR 16966, Apr. 8, 2003; 69 FR 5710, Feb. 6, 2004]