Attachment application.pdf

This document pretains to SAT-LOA-19960610-00080 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA1996061000080_1161382

WILLKIE FARR & GALLAGHER Washington, DC New York London Paris June 26, 1996 Mr. Harold J. Ng Chief, Satellite Engineering Branch Federal Communications Commission International Bureau Satellite & Radiocommunication Division 2000 M Street, N.W., Room 512 C Washington, DC 20554 Re: AP—4 Submissions for 77° W.L. and 81° wW.L. Dear Mr. Ng: W’ Loral Space & Communications Ltd. recently submltted applications for authority to construct, launch and operate geosynchronous communications satellltes in the fixed satellite service at 77° W.L. and 81° W.L. using portions of the C and Ku—bands at 77° and the Ku—band at 81°.1 Loral‘s proposed satellites will offer service to almost all of North and South America. Loral has developed the attached ITU AP—4 advance publication data for the proposed orbital locations. Pursuant to our telephone conversation, we are submitting these forms in the hope that we will be able to develop an appropriate filing for submission to the ITU. By filing the enclosed AP—4 forms, the United States will protect its interests by ensuring that the orbital locations identified remain available for use by US—licensed satellite systems. 1 Technical details of Loral‘s proposed systems can be found in Loral‘s applications filed June 10, 1996, FCC File Nos. 125—SAT—P/LA—96 and 126—SAT—P/LA—96. Three Lafayette Centre Telex: RCA 229800 1155 21st Street, NW WU 89—2762 Washington, DC 20036—3384 Fax: 202 887 8979 202 328 8000

Mr. Harold J. Ng June 26, 1996 Page 2 Thank you for your attention to this matter. If you have any questions or concerns, please do not hesitate to contact the undersigned. Sincerely, »//':/"/,«’;,/ 2c eeel e zt <. e uee_———w__~—_ w x=~ — Michele R. Pistone Andrew R. D‘Uva Counsel for LORAL SPACE & COMMUNICATIONS LTD. Enclosures

DATE FORM OF NOTICE AP4 ..u-.n.- (Day/Month/Year) PAGE 1 OF SATELLITE NETWORK setamaeserT Serial Number {APPENDIX 4) NOTIFYING ADMINISTRATION RR1042 RR1047A NOTIFICATION INTENDED FOR Advance Request for Assistance ADD MOD SsUpP [UulIs]al{M T1 Publicati of the iFRB C IFRB IDENTIFICATION NO OF NETWORK m TO BE MODIFIED/SUPPRESSED B: CHARACTERISTICS OF THE NETWORK 1 NAME OF THE SPACE STATION ‘UlSlAlS}A]T]-IZI‘flQl L 1 T T [ T T T Number 2 DATE OF BRINGING INTO USE 30fl goin;h 3 LSTE)“ :5*322:‘25;‘3:2?::53:;“‘“ SECTION ’AIRH 11 l;[AI;H ] l ! 3a ADMINISTRATIONS IN GROUP LL 3 LULO(C] T T ] T L [( 3b OPERATING AGENCY OR COMPANY _[1]2]0] 3c ADMINISTRATION RESPONSIBLE FOR THE STATION 4 ORBITAL INFORMATION a. FOR GEOSTATIONARY SATELLITES 1. NOMINAL ORBIT LONGITUDE 2. LONGITUDINAL TOLERANCE 3. 4. vistBiLtty arc 5. SERVICE ARC Degrees INCLINATION Degrees Degrees Degrees To West To East Degrees From W_ EM To E E/ From W__ EM To E_ EM [7]7le[olo|w olelolsl|{olelo|s] [Olelols 1lol4a|wil 15]3 W 1 lo[4lwil 75 [3 w 6. REASON FOR SERVICE ARC < VISIBILITY ARC ATTACHED L—_L—:] b. FOR NON—GEOSTATIONARY SATELLITES . 2. PERIOD 3. APOGEE 4. PERIGEE 5. CELESTIAL 8. NUMBER INCLINATION Days D Hours BODY OF SATS. Degrees Hours H Min. (kmi [kmj D Dj l I.] GENERAL NOTES : This form of notice consists of four parts — 1, 2, 3, and 4. in each part, each information item/data field includes a number in its label. This number is the same as that used for the same item in Appendix 4 (ORB—88) within the same part. For example, on the page labelled "Form AP4 — 2" (at the bottom), the field "4a1. Maximum power density" is the first item in section (a) of the paragraph numbered 4 in Part C. The items from parts F and G of Appendix 4 have been included in the parts C and D referred to above. The items from these parts have the letters F and G {correspondingly) preceding the number that is included in their labels. i. Data items that are related are grouped together in a box. For example, the page labelled "Form AP4 — 2" (at the bottom) contains a box titled "Emissions and power characteristics". It is possible to specify 6 different emissions with the associated power and power density information in this box. If there are more emissions, use another page of the same type to provide additional data, after checking ( X ) the field labelled "More emissions on next page" on the preceding page. In all cases where there is more information than can fit in a box, follow this procedure. iit. This form can be used to add to, modify or suppress an existing station, by checking the corresponding box at the top right— hand corner of this page in the area titled "Notification intended for". in the case of a modification of an existing station, where certain data fields are to be added, modified or suppressed, provide ALL the data in the particular box as they would look after the change. in addition, indicate that the corresponding beam, associated station or frequency range valus is being modified by entering M in the field that has been provided for this purpose at these levels. . Certain fields in this notice form have a superscript "1" as part of their labels. This has the following meaning : 1 — This information is to be provided only if available.

C: SATELLITE NETWORK CHARACTERISTICS IN THE EARTH—TO—SPACE DIRECTION ree [0]2] « [1](5] SATELLITE RECEIVING ANTENNA BEAM DETAILS ADD/MOD/SUP 5. CHARACTERISTICS OF THE BEAM of the beam b. RECEIVING BEAM DESIGNATION fi. NOTE: For a steerable beam, the third character of the beam designation shall be "R" OLD BEAM DESIGNATION (if changed) Djj ANTENNA +/4 dBi c1/d1/f1. MAXIMUM ISOTROPIC GAIN ; 3 ] 5’1’.[ o 1 c2/d2. ANTENNA GAIN CONTOURS DIAGRAM u. PoLAR ATTACHED sEE FiGuRE No . e/f2. ANTENNA RADIATION PATTERN DIAGRAM h. ESTIMATED ANTENNA GAIN DIAGRAM Vs ORBIT ATTACHED SEE FIGURE NO LONGITUDE ATTACKED SEE FIGURE NO INFORMATION TO BE PROVIDED FOR THIS RECEIVING ANTENNA BEAM 6. RECEIVING SYSTEM NOISE TEMPERATURE ofstation ofsenvice ersramew, LCO isamee O _TT610]0] xoi« oF Station CD] MWE aF starion 1J aF ochvice TD reRIOD ofF vatidiTy Years rsevema CCDOCLCOC—OCDOCCDOC—COCCOCCD «_ emspess 3/Fb. FREQUENCY RANGE WITHIN WHICH THE CARRIERS WiILL BE LOCATED Add/Mod/Sup FREQUENCY k/MIG IFRB IDEN‘TIFI(‘:ATION NUMBER of the freq. range Hz for modification/suppression rrom| [ Tela«lT2Islelolol T TJM TT To CJ CTeT7T2Istelo|o] T M T INFORMATION RELATED TO THE ASSOCIATED TRANSMITTING STATION(S) 8. MODULATION omm——Ep—asrcemes1 EMISSIONS AND POWER CHARACTERISTICS ChHaRAcTERisTics [3leImlo[FIxIFL I_] [+]3lole[0] [—[3[3le[o | l | |of LL | [3le6 Im{oim[7M 1| _| [+][3lole[0] [—l4[1lela] [ 1 _1 lel_}] [ 1 1 lel | L]_] [sle6IKl3IFIsIM |_] [+] T2le[0] [—I3[7lele] [ I[ [ lel ] [ I [ lel ] [ L1 [ [ 1 [ [ 1| ) L{Llel ] L[_I lel ] L1 [ lel ] [ | lel | L]_] TL T [ T T [ 1 [ } L [ lel ] L[ [ lel ] L I_I lel_] L [ | lel | L1 L1 T1 [ [ [ [ ) L[ [ lel ] LL [ Tel ] LI_[lel ] [_[ 1 lel ] LL | F. SPACE STATION fi?x?fi:i‘:" EARTH STATION Ag‘zx‘:g:i:’” ...ofarormonimeo0 mxebielareLCO l l l [ ' ' l l [ ] l j ! l [ ' L! I l ! 4b1. RADIATION PATTERN (give reference pattern or provide diagram} [rRlele!l—[Islslo| | | [ [ ] snenvetAoremmanes L ab2. AnTENNA RAPAToN CCinAarenyg., L_L_] wnext pace D MoRE AsSOC. TRANSMITTING MORE EMISSIONS ON STATIONS ON NEXT PAGE REMARKS: NOTES ON FILLING IN THIS PAGE FOR EACH BEAM FIRST FILL IN THE BOX TITLED ‘CHARACTERISTICS OF THE BEAM‘. FOR EACH EARTH—TO—SPACE SERVICE AREA ASSOCIATED WITH THIS BEAM, FILL IN THE UPPER PORTION OF THE BOX TITLED ‘INFORMATION TO BE PROVIDED FOR THis RECEIVING ANTENNA BEAM‘. FOR EACH SIZE (TYPE) OF TRANSMITTING EARTH STATION ANTENNA, FILL IN THE PORTION OF THE BOX TITLED ‘INFORMATION RELATED TO THE ASSOCIATED TRANSMITTING STATIONIS)‘, USE ADDiTIONAL PAGES AS NECESSARY. IF THIS IS A SPACE—TO—SPACE RELAY, IDENTIFY THE OTHER SPACE STATION(S) IN

C: SATELLITE NETWORK CHARACTERISTICS IN THE EARTH—TO—SPACE DIRECTION prace [0|3] or SATELLITE RECEIVING ANTENNA BEAM DETAILS ADD/MOD/SUP 5. CHARACTERISTICS OF THE BEAM of the beam b. RECEIVING BEAM DESIGNATION m NOTE: For a stearable beamn, the third character of the beam designation shall be "R" OLD BEAM DESIGNATION {if changed) [:D:] ANTENNA +/4 dBi c1/d1/f1. MAXIMUM ISOTROPIC GAIM 4. 3 r.fl.l 4 1 c2/d2. ANTENNA GAIN CONTOURS DIAGRAM 0. POLARIZA ATTACHED seE Figure No |_12] eif2. ANTENNA RADIATION PATTERN DIAGRAM h. ESTIMATED ANTENNA GAIN DIAGRAM vs ORBIT ATTACHED SEE FIGURE NO LONGITUDE_ATTACHED SEE Figure No INFORMATION TO BE PROVIDED FOR THIS RECEIVING ANTENNA BEAM asu: ss, D ssm CD TTeTs]0] «w 8. RECEIVING SYSTEM NOISE TEMPERATURE us69 »=s, 0 ssm O #$8, D #MWME D]] rmwowor 2@« iservicearea [_[ [ |[ [ [ I[ [ | J( T T [ T [ }[T [ C T T J [ [ J ca stavceamerpagnan 3/Fb. FREQUENCY RANGE WITHIN WHICH THE CARRIERS WILL BE LOCATED Add/Mod/Sup FREQUENCY k/MIG IFRB IDEN.'I"IFI(':ATION NUMBER of the freq. range Hz for modification/suppression rrom| [_] [ 1 T TAlslel7Is]l | T ll(€] TT To C | [ T THikleolo|TTle@]| TT INFORMATION RELATED TO THE ASSOCIATED TRANSMITTING STATION(S) EMISSIONS AND POWER CHARACTERIsTiCS cimncreAboas, 8. MODULATION mompsone| oo ecesceagsen Ales Erxmomrw_ D | Eekes Elxisiem | T Te C CO [(2]7im|o[FIXIF!L [ 1 [+l2{4le[s] [—[3lsle(2] [_[ | lef } [ | | lel ] LL] [sleIKls|FlawmM_I_] [—[ Iz2lelo] [—]4l1lei6] [ I [ lel ] [_L | le[l ] (T] CTL T T T T TT T3 | LULTMe[ ] LTLTTe] LLTLe[] | LULTHel] L T L T [ [ 1 T [ } | L [el ] 1 [ e ] L [ [ lel ] L1 _I lel ] LCL] L1 [ [ 1 1 1 1 j LTL[lel] LL [ lel ] L [ [ lel | L|_I le[l | C F. SPACE STATION appmonisuP EARTH STATION Apomonisup *.Camceotmonnme0 npnonnasnriannnpsspne [|1[TUGTJ [ [ [( [ [ [( T 4b1. RADIATION PATTERN (give reference pattern or provide diagram} [rRlelel—Islslol [ [ | | | omnorige.oeArracimages d02. ANTENNA RAPATON 0CarrHogrengs L_L— SIONS ON NEXT PAGE D MORE ASSOC. TRANSMITTING moRE EMIS STATIONS ON NEXT PAGE REMARKS: NOTES ON FILLING IN THIS PAGE FOR EACH BEAM FIRST FILL IN THE BOX TITLED ‘CHARACTERISTICS OF THE BEAM‘. FOR EACH EARTH—TO—SPACE SERVICE AREA ASSOCIATED WITH THIS BEAM, FILL IN THE UPPER PORTION OF THE BOX TITLED ‘INFORMATION TO BE PROVIDED FOR ThHiis RECEIVING ANTENNA BEAM‘. FOR EACH SIZE [TYPE) OF TRANSMITTING EARTH STATION ANTENNA, FILL IN THE PORTION OF THE BOX TITLED ‘INFORMATION RELATED To THE ASSOCIATED TRANSMITTING STATION(S)‘. USE ADDITIONAL PAGES AS NECESSARY. IF THIS IS A SPACE—TO—SPACE RELAY, IDENTIFY THE OTHER SPACE STATION(S) IN

C: SATELLITE NETWORK CHARACTERISTICS IN THE EARTH—TO—SPACE DIRECTION ree (0]4] o [1]5] SATELLITE RECEIVING ANTENNA BEAM DETAILS ADD/MOD/SUP 5. CHARACTERISTICS OF THE BEAM of the beam b. RECEIVING BEAM DESIGNATION E NOTE: For a atesrable beam, the third character of the beamn designation shail be "R" OLD BEAM DESIGNATION {if changed) ED:) ANTENNA +4 aBi c1/d1/f1. MAXIMUM ISOTROPIC GAIN ; 3‘[0“(.[ 4 1 EL__[]:D c2/d2. ANTENNA GAIN CONTOURS DIAGRAM g. . POLARIZATION T1 ATTACHED SEE FiGureNo . e/f2. ANTENNA RADIATION PATTERN DIAGRAM h. ESTIMATED ANTENNA GAIN DIAGRAM VS ORBIT ATTACHED SEE FIGURE NO LONGITUDE ATTACHED SEE FIGURE NO INFORMATION TO BE PROVIDED FOR THIS RECEIVING ANTENNA BEAM 8. RECEIVING SYSTEM NOISE TEMPERATURE 28. CLASS - 2b. NATURE 22. CLASS Dj 2b. NATURE D::] _ Kelvi OF sTATION [EJC) or seavice [CIR) OF STATION or seavice L_L161519] evins 2a. CLASS D:] 2b. NATURE [:D 2a. CLASS ED 2b. NATURE ED PERIOD OF VALIDITY - OF sTaATION or senvice OF sTATION OF sERVIcE El ALID Yaeare iservice area [__| [][ | | J( | [ I( T [ ][ T T I T T N T T J( T | | oa seaviceamiapimcram 3/Fb. FREQUENCY RANGE WITHIN WHICH THE CARRIERS WILL BE LOCATED Add/Mod/Sup rREquENCY X/MIG IFRB IDENTIFICATION NUMBER of the freq. range Hz for modification/suppression rrom| [] |I T THisleIsTTU@®]| UOUTTTT] To O TT TiIke@olelTe TN INFORMATION RELATED TO THE ASSOCIATED TRANSMITTING STATION(S) EMISSIONS AND POWER CHARACTERISTICS cfmhgfigg,gfigg'és 7ma9.NecessanysANDWiDTHOR , #e2/te _ 441. MAXIMUM Powen 4«. MiniMuMcanRien) rarezb.SPACEIEAATH at7kohmantno! Ermomrw 0 Ezste@ Elzlsle® D l€l 1e TCO ErmoExE D EBEes® | CBlses CCCA )|C—GeHA| TD GekBErm O CCEeda cemes CCCA ltTeh|! 0 C—GCCGCCO—| ce |G—eaolHHealateal t C—CCCH—C—D a—Ben | a&—oe|H—GeHA|HHeAl t C—CC—G——OO—H| ce |H—eao)H—Hea)——t—eaAl t F. SPACE STATION Aff’ix‘:g:i:" EARTH STATION Aff[i’h“:‘:gii‘f ieolaaegso0 mMenlelatcL—i®xdl 1_GTTTT (Rl€lel—Islelol 11— 110 l ‘ l l l l ] l l I i { I I [ I ’ [ i [ l 4b1. RADIATION PATTERN (give reference pattern or provide diagram} mnpsenememeCD issmeronsnmernonooarrzenss T MORE ASSOC. TRANSMITTING MORE EMISSIONS ON NEXT PAGE D STATIONS ON NEXT PAGE REMARKS: NOTES ON FILLING IN THIS PAGE FOR EACH BEAM FIRST FILL IN THE BOX TITLED ‘CHARACTERISTICS OF THE BEAM‘. FOR EACH EARTH—TO—SPACE SERVICE AREA ASSOCIATED WITH THIS BEAM, FILL IN THE UPPER PORTION OF THE BOX TITLED ‘INFORMATION TO BE PROVIDED FOR THIS RECEIVING ANTENNA BEAM*. FOR EACH SIZE (TYPE] OF TRANSMITTING EARTH STATION ANTENNA, FILL IN THE PORTION OF THE BOX TITLED ‘INFORMATION RELATED To THE ASSOCIATED TRANSMITTING STATIONIS}‘. USE ADDITIONAL PAGES As NECESSARY. IF THIS IS A SPACE—TO—SPACE RELAY, IDENTIFY THE OTHER SPACE STATION(S) IN

D: SATELLITE NETWORK CHARACTERISTICS IN THE SPACE—TO—EARTH DIRECTION me: [o]5] «& [1]5] SATELLITE TRANSMITTING ANTENNA BEAM DETAILS ADD/MOD/SUP 5. CHARACTERISTICS OF THE BEAM of the beam b. TRANSMITTING BEAM DESIGNATION . NOTE: For a steerable beam, the third character of the beam designation shall be "R" OLD BEAM DESIGNATION {if changed) E]:D ANTENNA CHARACTERISTICS +/4 dBi c1/d1/f1. . MAXIMUM MAX ISOTROPIC GAi M L 2[6—.[.[8 1 D]]jj c2/d2. ANTENNA GAIN CONTOURS DIAGRAM 9. POLARIZATION ATTACHED SEE FIGURE NO L[4] e/f2. ANTENNA RADIATION PATTERN ED h. ESTIMATED ANTENNA GAIN DIAGRAM vs DIAGRAM orsit INFORMATION TO BE PROVIDED FOR THIS TRANSMITTING ANTENNA BEAM 22. CLaSS 2b. NATURE 28. CLASS 2b. NATURE of station oroauice LCIRI| 2s SAE CD] or sErvice CD] 22. CLaSS 2b. NATURE 22. class 2b. NATURE oF sTaTION CL or service oF sTtaTION C1 OF SERVICE LCL] PERIOD OF VALIDITY Years iservice amea [[ | ][ [ | |[ | [ }[ T T JC T T JC T 1J T T [ T [ } «s oa encarents 3/Fb. FREQUENCY RANGE WITHIN WHICH THE CARRIERS WILL BE LOCATED Add/Mod/Sup rREéqueNcy K/MIG IFRB IDENTIFICATION NUMBER of the freq. rang Hz for modification/suppression rrom| [] |[Tsl4lololelolol T m TT To C | IsIzlololeolo[ T lJm TT SPACE STATION EMISSIONS AND ASSOCIATED RECEIVING STATION(S) INFORMATION EMISSIONS AND POWER CHARACTERISTICS chHanretEmstice (3IsImlo[EIxIEI [_] [+]1]4le[7] [—[4[slel3 |_lel L le] C1 (3lsimlolu[GMWM _1 | +[1]4le[7] —IslzleA] L | L| [ [s[elx[3[rlsMWM [ _] [—[1[7le[a3] [—Islglelal L1_I_lel ] [I [ lel |] L1 T T T T T T [ [ | LL[e[ ) LULT[ eC ) | TL T lel ] [ 1| lef ] LCL] T T T T T T [ [ | LT [el ] T [ e[ | LIL_{LLlel j L 1| _I lel | CL] C T T T T T T [ [ } L [e[ ] | TL T He[ | LLI[_e[ ] [ | I le[ } e F. SPACE STATION ADD/MOD/SUP EARTH STATION ADD/MOD/SUP CHARACTERISTICS OF RECEIVING SPACE of the station of the station STATIONS FOR SPACE—TO—SPACE RELAYS DESIGNATION OF TYPICAL EARTH STATION a. SPACE STATION NAME [Tly[p|rlelalcl—lel 1 1 1 [ [ [ | [ [ [ ] CEAAA AACAOAAATTTTD ] * HOERPPNTEHGuscsawen . o tE G3e. BEACON AND TELEMETRY INFORMAT [rlielel—[slslo| [ [ | | TEMPERATURE ATTACHED. SEE ATTACHMENT NCL: Kelvins afz. antenna raniation piacramarractien 10 T |1}slo MoRE EMiSSIONS ON NEXT PAGE D mone assoc. rEcEiviNG STATIONS ON NEXT PAGE REMARKS: NOTES ON FILLING IN THIS PAGE FOR EACH BEAM FIRST FILL IN THE BOX TITLED ‘CHARACTERISTICS OF THE BEAM‘. FOR EACH SPACE—TO—EARTH SERVICE AREA ASSOCIATED WITH THIS BEAM, FILL IN THE UPPER PORTION OF THE BOX TITLED ‘INFORMATION TO BE PROVIDED FOR THis TRANSMITTING ANTENNA BEAM*. ALSO PROVIDE THE "EMISSION AND POWER CHARACTERISTICS® FOR THIS TRANSMITTING ANTENNA BEAM. FOR EACH SIZE (TYPE] OF RECEIVING EARTH STATION PROVIDE THE EARTH STATION DETAILS AS SPECIFIED. IF THIS Is A SPACE—TO—SPACE RELAY, IDENTIFY THE OTHER SPACE STATION(S) IN THE

D: SATELLITE NETWORK CHARACTERISTICS IN THE SPACE—TO—EARTH DIRECTION race [O[6] or SATELLITE TRANSMITTING ANTENNA BEAM DETAILS ADD/MOD/SUP 5. CHARACTERISTICS OF THE BEAM of the beam b. TRANSMITTING BEAM DESIGNATION NOTE: For a steerable beam, the third character of the beam designation shall be "R" OLD BEAM DESIGNATION (if changed) E:[]:j ANTENNA CHARACTERISTICS + /4 dBi c1/d1/f1. MAXIMUM ISOTROPIC GAIN + 31le]4] e.roranization * T c2/d2. ANTENNA GAIN CONTOURS DIAGRAM ATTACHED SEE FIGURE NO e/f2. ANTENNA RADIATION PATTERN DIAGRAM CL h. ESTIMATED ANTENNA GAIN DIAGRAM VS ORBIT INFORMATION TO BE PROVIDED FOR THIS TRANSMITTING ANTENNA BEAM 2a. CLASS - 2b. NATURE - 2a. CLASS ’:D 2b. NATURE Dj OF STATION OF SERVICE m OF STATION oFr seavice 2a. CLASS ED 2b. NATURE ljj 2a. CLASS D’_‘] 2b. NATURE Dj PERIOD OF VALIDITY Years OF SsTATION oFr seavice OF STATION or seavice iservicearea [_| [ ][ [ | |[ [ [ 1( [ T [ [ T( [ T J( T [ [ [ ||as SERVICE AREA DIAGRAM ATTACHED CLD] 3/Fb. FREQUENCY RANGE WITHIN WHICH THE CARRIERS WILL BE LOCATED Add/Mod/Sup k/M/G IFRB IDENTIFICATION NUMBER FREQUENCY of the freq. rangef Hz for modification/auppression FROM C TT Til1lel«Islo]l TU[G) TN TO C T TTili]elzlolo]l TU[a] OO SPACE STATION EMISSIONS AND ASSOCIATED RECEIVING STATION(S) INFORMATION EMISSIONS AND POWER CHARACTERISTICS 8. MODULATION [217imloiml7zWM_|_] [+]2I1lele) [—[4[gle[2 |_|el |_lel L_L} (27imlolrlx[rIL 1J ~\2zlilels] —I4l1lel4] I[LTeD)] [ ILILe| D [sTel«xI3IrI3MWM 1 ] —LTsglel2] [—I4Isleis} TT Te 1| Te [ LII T T T [ [ T j LUL [ el ] L I[ e ] LL _T lel ] [ L [ lel } EB L1 I L T 1 1 [ [ j LTL[el ] L1 [lel ] | L T lel | [L_L_| lel | CT] TT [ T [ T [ | } L [ [ le] ] L1 [el ] L T _lel |] L1 L _lel } mH F. SPACE STATION Appmon/sup [~~] EARTH STATION ADD/MoD/SuP of the station CHARACTERISTICS OF RECEIVING SPAcE of the station STATIONS FOR SPACE—TO—SPACE RELAYS DESIGNATION OF TYPICAL EARTH STATION a. SPACE STATION NAME [tTIyTrTi{elalr] — Ilul [ [ [ [ [ [ T T T J L1 T T T T T T J T [ T | T T T [ [ T T j 8b1. RADIATION PATTERN {give reference pattern or provide diagram} 8a. RECEIVING SYSTEM NOISE G3c. BEACON AND TELEMETRY INFORMAT! [rlele[—Is[s8lol | 1 | | | TEMPERATURE ATTACHED. SEE ATTACHMENT NO.: Kelving BH 2. ANTENNA RADIATION DIAGRAM ATTACHED SEE FIGURE NO.: L ] _ Islolo MORE EMISSIONS ON NEXT PAGE D MORE ASSOC. RECEIVING STATIONS ON NEXT PAGE remanrksIRANSMISSIONS IN THE BAND 11.45—11.70 GHz WILL MEET THE REQUIREMENTS OF RADIO REGULATION APPENDIX 28. NOTES ON FILLING IN THIS PAGE FOR EACH BEAM FIRST FILL IN THE BOX TITLED ‘CHARACTERISTICS OF THE BEAM‘. FOR EACH SPACE—TO—EARTH SERVICE AREA ASSOCIATED WITH THIS BEAM, FILL IN THE UPPER PORTION OF THE BOX TITLED ‘INFORMATION TO BE PROVIDED FOR THIS TRANSMITTING ANTENNA BEAM*. ALSO PROVIDE THE "EMISSION AND POWER CHARACTERISTICS" FOR THIS TRANSMITTING ANTENNA BEAM. FOR EACH sIZE (TYPE) OF RECEIVING EARTH STATION PROVIDE THE EARTH STATION DETAILS AS SPECIFIED. IF THIS Is A SPACE—TO—SPACE RELAY, IDENTIFY THE OTHER SPACE STATIONS) IN THE

D: SATELLITE NETWORK CHARACTERISTICS IN THE SPACE—TO—EARTH DIRECTION mee [O][7] o [1]5] SATELLITE TRANSMITTING ANTENNA BEAM DETAILS ADD/MOD/SUP 5. CHARACTERISTICS OF THE BEAM of the beam b. TRANSMITTING BEAM DESIGNATION NOTE: For a steerable beam, the third character of the beam designation shall be "R" OLD BEAM DESIGNATION (if changed) E:[:D ANTENNA CHARACTERISTICS +/ dBi c1/d1/f1. . MAXIMUM ISOTROPIC T G, AIN 4 3[0 l @| l 4 1 ED:I:D c2/d2. ANTENNA GAIN CONTOURS DIAGRAM 0. POLARIZATION ATTACHED SEE FIGURE NO e/f2. ANTENNA RADIATION PATTEARN h. ESTIMATED ANTENNA GAIN DIAGRAM VSs DIAGRAM oRsit . INFORMATION TO BE PROVIDED FOR THIS TRANSMITTING ANTENNA BEAM 22. class 2b. NATURE 22. CLass 2b. NATURE of station or senvice E@ or station D:] ofr seavice D:I 2a. CLASS 2b. NATURE 2a. class 2b. NATURE of sTation D:] OF SERVICE ED OF sTATION ED or seavice [D PERIOD OF VALIDITY Years i:seviee asea CJ—TOLOLTOCLOCLTOCTDOLCTOLCLCDODLCT T on severenpaeram 3/Fb. FREQUENCY RANGE WITHIN WHICH THE CARRIERS WiILL BE LOCATED Add/Mod/Sup FREQUENCY /M/G IFRB IDENTIFICATION NUMBER of the freq. range] Hz for modification/suppression rrom| [] T T Thlel«Islo] T[{e@l TT To CJ C T Tmelzlolol |@ TITTT] SPACE STATION EMISSIONS AND ASSOCIATED RECEIVING STATION(S) INFORMATION EMISSIONS AND POWER CHARACTERIsTiCS Crianacteristics rescrowes uio s_~ — .R.P;’— 1_| atracHiment no. (217imloiml[7zM_|_] [+l2Iilele] [—{4lglel2 |_le] L_{ol CL] [217im[lolrF[xIrEI | J [+l2[tlefe] [—l4Imlela] TL lel ] [L[_[lel ]| [{_L] (slelxlsirIslw 1 ] [—] lTglel2) [—l4]slels] [ [ l lel ]| [ [ [ lel ]| [ 1 C T T T T T TJ LLel ] LLTIe] LULTLIe ] LLTel] L L 1 1 [ J 1 [ J L T el ] [|1 [ el ] LI[L[|el ] L [ [ lef ]| [_[] U T 1 [ J 1 [ J L [ _Dlel}j J [ e ] L L1 lel ] L | Ilef ] CL] F. SPACE STATION ApoMopisuP EARTH STATION atthestation ...ounnponue00 m elan]—I€lul [ G—TTTTO L 1 I I I I 1| { [A { 11A I [ IT [ AO] sen maotarioneatrea®t ) _( () ge. RECEIVING G3c. BEACON AND TELEMETRY INFORMAT lRIElC['IBIB]O! l l [ l ’ i‘éa“;?gg%‘sg ATTACHED. SEE ATTACHMENT NOL: B}2. ANTENNA RADIATION D'AGZQ?F'AGTUY:EC::SD L_LJ l E-E)l O MORE EMISSIONS ON NEXT PAGE D MORE ASSOC. RECEIVING STATIONS ON NEXT PAGE remankssTRANSMISSIONS IN THE BAND 11.45—11.70 GHz WILL MEET THE REQUIREMENTS OF RADIO REGULATION APPENDIX 28. NOTES ON FILLING IN THIS PAGE FOR EACH BEAM FIRST FILL IN THE BOX TITLED ‘CHARACTERISTICS OF THE BEAM‘. FOR EACH SPACE—TO—EARTH SERVICE AREA ASSOCIATED WITH THIS BEAM, FILL IN THE UPPER PORTION OF THE BOX TITLED ‘INFORMATION TO BE PROVIDED FOR THis TRANSMITTING ANTENNA BEAM*. ALSO PROVIDE THE "EMISSION AND POWER CHARACTERISTICS® FOR THIS TRANSMITTING ANTENNA BEAM. FOR EACH SIZE {TYPE) OF RECEIVING EARTH STATION PROVIDE THE EARTH STATION DETAILS As SPECIFIED. IF THIS IS A SPACE—TO—SPACE RELAY, IDENTIFY THE OTHER SPACE STATION(S) IN THE

E. OVERALL LINK CHARACTERISsTICS pace [G@|Q] or FOR GEOSTATIONARY SPACE STATIONS USING SIMPLE FREQUENCY—CHANGING TRANSPONDERS AND OPERATING WITH EARTH STATIONS ONLY E1. Indicate the strapping (connection) between the uplink and downlink frequency bands for each intended combination of receiving and transmitting beams Serial Appysur BEAM.COMBINATION FREQUENCY BAND COMBINATION 18 fi; ‘:'t‘h' UPLINK pownLink UPLINK wmIG DOWNLINK mic| BAND * rep BEAM BEAM FREQUENCY BAND Hz FREQUENCY BAND Hz Limits [0] [] [erle[] [TleT [ 6lal2ls|elo| | | ] lim] [ [sl4lolole{O| | | | IIm] reom | 6l7!2ls|elo| | | | lim} [ |sl7lololelo| | | | |im]| to { [RIKI IKD]]| TT TilslelzIslol T To) TT Tililel4Is]o]| T1 IG]| ow [ 1 | [il4lelololo{l | lia): [ _1 | |1l1le{7{lolo| | llG]]| t [ [elxl2l] [I«kT2l| LULT TiTsTel7Islol T lgl : TL T Til1]e{4[slo|l 1 [[G]| mom [ [ T1[f4l]elololo]l | IIG] LL_I Ti]ilel7lolol [ IG]| 3 [elxD]} [TiKI2]]| LTL T TiTslel7Islo[ T IG)]: L T Til1lel4[slo] | |G]| mou _1 I l1il]l4jelololol | IIa): [ _1 | l1lilel7lolol | IIG]| t [olo{s]| [ [erlxl2] [1ix[1] LL T TAIsTel7zIslol 1 lig] _T 1 Ti1l1lel4lslo]| | |IG]| on [ [ Ti[4]elololol 1 IG)]: [ I T1l1le[7lolol | IIG]| t T719 | UE OTT3] TT T T Te T T T T T 3 LUTLT T T Te T T T T [[ ]| ow CT T T T Te T T T T T); TT T T Te T T T T [ ]| t {TTJ] Q U OM UTLT T T Te T T T T [ ): LTT T T Te T [ T T [[ ]| m®on C [ T T Te T T T { [( j :; TL [ T T lTel [ [ T [[}]| 1 T709 C U TT 3| UCTUTTTTTIe TT T T [3 TT T T Te T T T T [ ]| on [ [ [ T [ e T T T [ [ ;i L [ 1 [ lel [ [ [ [ [ ]| 1 MORE ON NEXT PAGE D E2. For each entry (or group of entries) in table E1 indicate the following equivalent satellite link noise temperatures and associated transmission gains. If these values are specific to an associated receiving earth station, provide its name. Reference to Serial .1'L°SVX$-ST EC ‘Z.J;SQ’NCSI%SDNN b:j‘,g%:x bz.ATsimslr‘fg)NN ASSOCIATED RECEIVING EARTH STATION DESIGNATION No{(s)}. in table E1 LINK NOISE TEMP. WITH ai HIGHEST RATIO WITH b1 Keivins +1D____ 48 OF FaHSCSE T. /| as C1 T }OUILLJJLL N11 L le JJ[ I | | | | [ let |J [ _1 1 1 T 1 1 1 [ 1 [ | 1 [ [ ] CT T J [ [ J{ULLT O 1 fet JI[ 1 [ [ [ [ lel | [ 1 [ [ T 1 [ 1 [ | [ [ [ [ [ ] CT T 3O T DL T T | | lef ]1[ [ I | [ } [lef ]| [ I T |1 [ 1 T [ [ [ T [ T [ [] T T }{L [ LGILL T | | L le ]J[ _T [ 1 1 ) Je 1| L L L 1 T T [ [ T [ [ [ [ [ ] C T T 3O [ TCO T U L lel 11L [ [ T 1 1 lel | L L T T T T [ [ T [ [ T [ [ [ ] CT T HOT T JILT _T 1| L e J1[ I [ [ [ ] [ Te |] L [ [ T [ T [ T | [ [ T T [ J U T }HOLJLL T | | _ lel JJL TL [ L [ ) [ lef ]| [ [ [ T [ T T T T [ T [ [ [ CT 3O O(C](ULT 1| L e ]I[ | [ [ [ | [ lel 1| [ L 1| [ [ [ [ [ [ [ [ [ [ [] C T G—L TL DL T 1 L lel ]J[ I [ [ [ L let | L L T T T T [ 1 T [ [T T T O LC TJOOJ LIL T | L lef JJ[ |I | [ [ ] L lel |] [ T [ [ T1 [ [ T [ [ T | [ T [] _ _ L L 1 UOIILULL L 1| L el 1J _T T [ 1| L lel }| [ 1 [ 1 [ 1 1 1 1 1 11 [ [ [ MORE ON NEXT PAGE D

Figure 1. USASAT—24Q Space Station Receive Antenna Gain Contours Beam RC Orbital View From 77 Degrees West Latitude and Longitude Lines at 10 Degree Intervals 10 100 49 s0 70 ep so Lo | C C inLT_TVrefe > o LfiLN3 »AE R Z B E — A — T3‘ — \X\ 20 f —10 —20 Notes: 1. Contours shown are —2, —4, —6, —10, —15, and —20dB relative to maximum gain. 2. Maximum isotropic gain is +25.9 dBi. 3. Does not include antenna pointing error of £0.1° worst case. 4. x Denotes subsatellite point. 5. + Denotes peak gain.

Figure 2. USASAT—24Q Space Station Receive Antenna Gain Contours Beam RK1 Orbital View From 77 Degrees West Latitude and Longitude Lines at 10 Degree Intervals Boresight 98.2W x 32.4N @_‘o“‘-“_—.‘-—.-..---——-~—-.‘ «— ‘o“"‘o:-/' ~ # 18 L. e on h 993 h: seseae centnh8900EE ces se s ceaen ene,, ¢& ,I L2kn % a s 18 9 a . .* ~& @ 1 2 N ~ ,’ 28 e# > = T — «/ © en -../ h €s2 5 o. 2 +4 . .: = LE & a '..' \ * c, a 7 28. . a4 . 4BA Z * NC q \ t ult 210 io 5. A ? 1 i * f .GA. \ / ’-z 4 ? ,' / = T . ..' .o’. 1. Contours shown are —2, —4, —6, —10, and —20dB relative to maximum gain. 2. Maximum isotropic gain is +31.4 dBi. 3. Does not include antenna pointing error of +0.1° worst case. 4. x Denotes subsatellite point. 5. + Denotes peak gain.

VS 1b GCT Figure 3. USASAT—24Q Space Station Receive Antenna Gain Contours Beam RK2 Orbital View From 77 Degrees West Latitude and Longitude Lines at 10 Degree Intervals Boresight 62.1W x 12.5S ~SD | —wl_\__\ 4 /~ z2 1. Contours shown are —2, —4, —6, —10, and —20dB relative to maximum gain. 2. Maxium isotropic gain is +30.4 dBi. 3. Does not include antenna pointing error of£+0.1° worst case. 4. x Denotes subsatellite point. 5. + Denotes peak gain.

Figure 4. USASAT—24Q Space Station Transmit Antenna Gain Contours Beam TC Orbital View From 77 Degrees West Latitude and Longitude Lines at 10 Degree Intervals HO 109 910 #D T70 60 50 ud ::- \,»\ ’-“l.—-—’.—-—{.-“/ 4o " _.w_wZ, 20 J 20 10 —10 — 30 —40 —— 50 K Notes: 1. Contours shown are —2, —4, —6, —10, —15 and —20dB relative to maximum gain. 2. Maximum isotropic gain is +26.8 dBi. 3. Does not include antenna pointing error of +0.1° worst case. 4. x Denotes subsatellite point. 5. + Denotes peak gain.

Figure 5. USASAT—24Q Space Station Transmit Antenna Gain Contours Beam TK1 Orbital View From 77 Degrees West Latitude and Longitude Lines at 10 Degree Intervals Boresight 98.2W x 32.4N .+ sseses c t ****re se se en s ........... mg \ 1. Contours shown are —2, —4, —6, —10, and —20dB relative to maximum gain. 2. Maximum isotropic gain is +31.4 dBi. 3. Does not include antenna pointing error of +0.1° worst case. 4. x Denotes subsatellite point. 5. + Denotes peak gain.

Figure 6. USASAT—24Q Space Station Transmit Antenna Gain Contours Beam TK2 Orbital View From 77 Degrees West Latitude and Longitude Lines at 10 Degree Intervals Boresight 62.1W x 12.58 90 6N. 10] i ao col\_—\ hxz nen Notes: 1. Contours shown are —2, —4, —6, —10, and —20dB relative to maximum gain. 2. Maxium isotropic gain is +30.4 dBi. 3. Does not include antenna pointing error of£0.1° worst case. 4. x Denotes subsatellite point. 5. + Denotes peak gain.

Figure 7. USASAT—24Q . Space Station Located 77 Degrees West Gain Towards the Geostationary Satellite Orbit for Beams RC and TC 30 NJ o I Antenna Gain (dBi) wa o I o o wa s —20 1 h 1 1 i 1 1 1 N 1 1 L i 1 M i i 0 20 40 60 80 100 120 140 160 180 200 220 240 260 280 300 320 340 360 East Longitude (deg) Figure 8. USASAT—240Q Space Station Located 77 Degrees West Gain Towards the Geostationary Satellite Orbit for Beams RK1, RK2, TK1 and TK2 40 30 |— Antenna Gain (dBi) 10 |— -20 T 1 _L 1. 1 1 1 1 1 T L T 1 1 . T 1 0 20 40 60 80 100 120 140 160 180 200 220 240 260 280 300 320 340 360 East Longitude (deg)


Document Created: 2016-12-13 18:38:01
Document Modified: 2016-12-13 18:38:01
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