Attachment response

response

SUBMISSION FOR THE RECORD submitted by Celsat

response

2004-11-04

This document pretains to SAT-MOD-20040717-00134 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2004071700134_405602

Skappen, Arps, State, MeaGHeR & FLOM LLDRlG‘NAL 140 new yone avenue, nw wekmeton. oc 200082111 wl rugosar—r0ee Meceiveg BEZ. rax gozi 3032760 ho wnnustagdencom NOY q 4 2004 Fewnl Pollcy Brangh se MMematonalBureay Musue November4, 2004 peEoEjJVED 3s%. NOV ~ 4 2004 Marlene Dortch, Secretary Federal Communications Commission a 445 12th Street,S.W. 12th Street Lobby, TW—A325 Washington, DC 20554 RE: Celsat America, Inc. Dear Ms. Dortch: Enclosed on behal of Celsat America, Inc.("Celsat*), please find the two most recent monthly progress reports issued by Space Systems/Loral, Inc. (*Loral®)in accordance with the satellite manufacturing contract pursuant to which Loral is building Celsat‘s satellite. This submission responds to a letter dated October 27, 2004 to the undersigned counsel from Fem Jarmulnck, Deputy Chiefof the Satellite Division ofthe Commission‘s Interational Bureau. Please contact the undersigned should you have any questions concerning this submission. Sincerely, 3 wR &LLL~z #lk. Brign D. Weimer Counsel to Celsat Enclosures cc: Fem Jarmulnck Alyssa Roberts s12000seeca usw

Celsat Monthly Progress Report For September 12, 2004 a.. Major Program Events: * Contract amended 712704 for new satellte design. * Finalized amendment to contract documents. Documents approved and signed: — Amendment 1 to Celsat Contract —— Exhibit A, Statement of Work —— Exhibit B, Spacecraft Performance Specification —— Exhibit C, Product Assurance Plan: —— Exhibit D, Satellte Program Test Plan * Supported Celsatsubmission of FCC Form 312. Performed initial satellte budget and performance predictions to support filing.. Included antenna analyses, payload design, bus configuration and sizing, and TT&C link analysis. * Established Program Management Office for the Celsat program. Provides Celsat customer interface and interal company direction. Completed price validation exercise. Allocated 32,000 Ssolar cells from inventory for use on Celsat solar arrays as part ofstart of construction activities. Cells are stored in Japan at manufacturer and will be available for solar array construction * Initial assessment of facilities and factory processes for Celsatstarted. The Celsat satellte is expected to present no difficulties for production handling and test as it is very similar to other programs completed by SS/L. * SS/L is 180 9001 certified. Standard quality plans and procedures are approved for all programs. A review ofthe applicability ofthese standard plans and procedures has been initiated. * Performance budgets and qualifiation status lit are in development. Detailed results and compliance matrix are to be available at CDR per the contract. b.. Technical Status: 1. Spacecraft — See attached description for current design status summary. —— Preliminary mass, power, thermal, propellant analyses completed. Results show spacecraft is within normal design limits for satllite and Iaunch vehicles. —— Preliminary propellant analyses show positive mass margin to current budget. — Spacecraft will fit in 4m fairing compatible launch vehicle. — Working with 2 antenna suppliers for define iniial stowage and deployment interface requirements. — Spacecraft will y 20—30 degrees offearth—pointing normal to obtain FOV and optimum antenna configuration. 2.. Payload —The payload detailed design is underway. — Payload uses 12m unfurlable antenna with 48 element array for CONUS and AK coverage. Separate subarrays provide HI and PR/USVI coverage. Finalization of array Gelsa Fages Morthy Progress Repor 712004 yc LORAL

size based on coverage area, performance, repeater equipment factor, and configuration. 46 clements are used for transmit and 48 elements are used for receive. — Discussions with antenna suppliers started. — Repeater uses S—band TWITA with DRC. This allows improved de and thermal efficiency for same rf power. Penalty in mass and size versus previous SSPAs. — Repeater channelizes to full 20MHz MSS band to support ground—based beamforming architecture using analog S—band channelfilters. Gateways determine segmentation of the band for users. Single conversion between Ka and S—band simplifies repeater design. Modified versions of existing repeater units(filters, converters, ampliiers) are used to minimize NRE and achieve best schedule. — Developed generalized calibration and pointing coefficient methodology to support ground—base beamforming. Beamforming coelficients for each antenna feed element generated at gateways. "Quasi—user"terminals monitor satellite ransmissions and uplink testsignals to provide calibration information for coefficient compensation. — Detailed repeater equipment list being refined. Discussions with suppliers started. — S—band antenna peformance trades between GT, EIRP and C1 started. Optimizations for various seenarios of frequency reuse for capacity in process. Frequeney reuse for K = 3 thru 12 being evaluated. 3.. Bus— The bus detailed design is underway. —.— Bus structure chosen similar t iPStar program currently under construction. Enables reduced NRE while providing fexibility for payload equipment accommodation. — Initial layout and configuration studies started. Optimizing comm panel layout for payload performance, — Eliminated deployable radiatiors by use ofTWTA with DRC which reduced thermal demand to spacecraft significantly. — Evaluating ADCS and propulsion to support "canted" angle orientation ofplatform. Trades of wheel size and thruster locations underway. Will use standard 12N biprop thrusters for EWSK. No NSSK planned. — Baselined electical power to come from standard solar cell and NiH battery technology. Initil analysis of available power due to shadowing of solar array by antenna mesh based on lessons leamed from MBSAT program which also uses 12m antenna. — Current baseline for TT&C is to use C—band for orbitraising and contingency. C:—band is common and supported by numerous TT&C stations worldwide. Orbit mising interference TBD. On station TT&C will be thru Ka gateway beams. At least one gateway will be designated for spacecraft operations. .. Program Controls: 1. Schedule— Inital program schedule attached. Schedule supports FCC filing date to bring frequencies into use by Feb 17, 2007. Identification of eritical paths and validation of the overall schedule is underway. Mitigation plans for schedule risk items will be developed. Schedule driver expected to be 12m antenna subsystem including reflector and boom 2.. Major NCR Status— None CelsatManthy Progress Report 1204 Page2 LORAL

3.. Class 1 Waivers, Deviations — None. 4.. Status of Outstanding Action Items — See attached. 5.. Invoice Status — No outstanding invoices. Received Milestone Payment No. 5. 6.. Status of Contract Changes — None. Clsat Monthly Progress Report 1204 Pages LORAL

Celsat Spacecraft Key Features Uhindcaion zo uie $land Artcera Retbace 12imurtatie Fond 1t comertanay Kitond Aterna Reteaee Zmigd es 4wot/onds HPA Sand in syor mora Kotund saswses mta Mss amig D0 Powe s Wt TrermalOasipaton 39M tren rnmdopemys Patorm use reco O ass arstle 12n Ratece Servcn te 1?yous Eletrea Pover DGPove e taweo, Sole Arays 251+2Gate parlsporwng Baterien 222eal 176.A NH batores Promlbicn Bgmpelan, 2140ky tomgetark, 12008 trusies, NST DaaHandeg 9t Onee Supertnb ovaliun Astade Cored Asbenls hiline RlegLaner Gon,enand un semorn Sutntersira «£Odig NS Tremal Heatigen, henton lanies onentrefecors Meturisns 2 udararaydrve ssoniies Trie Cbanderitrainy, Knb onio cormand enenptn Lsrchvahices ProimSeaburch, are, Alos 2A Gaisat Monthly Progress Report ant2004 Page d

Primary EIRP Summary rex a=—ms on som oro im Irih cssn w se an na letrensaese lc earae wo smne «n "an haatin trurnanirone on Hivaiiitrointer P sn Mrossrene noien & Sa forrne ouseomecmreae a» Toh inmcamce ue P on prwiro neace a sa Een antgnmuee smm he bor a as emommmamamzo im on a sa Iermace i& in & as benine a n ce anewow omm m on & aa Rrove a 34 ermeuce a an mescries a ie butmominace a on bentearmnam isfos ow Hencumyomcs « se ‘Iematotam & sal es B sal leaters se imen am heraroas ar—ae Farse man w vas n romon a Cw Eemetanyme Pommes ie« me biego a Primary G/T Summary rearemuey zowe brtess es bat keun az « rtecer ons ana lenent ns aiso Eeao mre oso om «e ana W¥idgimer am «n lcirer i BW cone soo om «e ast e beo ant manaen ate berema ranm es s «a praseianp mtace are horwicumryTaennces s1 emaitstoten aisce Inctetrg reerany azsca hrtema Tonp @500 0 mor «ax lmocns« im « eonntuton ofpecesse s ater oz «a ht ons Picorntutcnns aro « Ie atariems ement im « N amage t cans mestat 0 an hrurea Omeiiy, c aso « lor, on mss «on eprctcatoncant 150 hn io ass GT eengs dEotam iroan mcserato0 mn ns Omctuy,on as « on cor 1sos «an Spectcaton cant 1soo «an ooc oos « Calsat Monthly Progress Repor 1204 fim PageS

Spacecraft Mass Budget Mass Risk Subsystem t to) % Structure asss| s38 70% Mechanisms 18. 0s 18% Propuision 1455 s2. 36% Electrical Power sseo| 420 36% Solar Array 1709 se 40% RepeaterTransponder Trea| T26 100% Communications Antenna 2029) 203 100% Tmac 166 0s 50% lancs 73. 15 20% Data Handling System se.7 310 38% Thermal Gontrol fres) 124 70% Electrical Integration 1300 o2 10% Spacecraft—Dry Nominal 2sri2] i7si 689% Spacecraft—Dry w Risk 27493 Spussralt Fover Batget Electteal Power (Watts Isuesystem Ts En se Payons ested) ssieal sstea ons was| uss| arsa mc cos| ces se hocs mas mes| 1e Propuiion so s sal ers 1sao) ises| neal rarmat seno! seeal seel bamess ors! soel szal svesveramtont Tanal —reseal —riess eatey Crarnoiorargny toss Tesl swos osctarr toss To LowYatage Commntr Losses saal sral seal Baten—PCU Hamess toss seal sracecramrora rereal —ameal —aises Scer Amy Gapaany (@ EL ie y sorl —omra sia ShadominLosses soss| ied lscr Aray Gapanity (snadouing incuded) esseal suesol lsouar anmay no.racume maron 134%| 103% SR raiue Conmainy (t ierr Greus) eral smeal lcAray Gapabity (EOL with Shacowingiratures) szaee) sre2) lsorar ammay worsr—case mrom asr| se [hamns batey Fove ez worst.case sartery so0 1os% frat GaFanro Gontngeney (ecorsy sos (worst—case sartery voo 730% Celsat Monthy Progress Report ant2l04 Page

Program Schedule Colsat Program Master Schocule vesuies 7 ma ronmrrnmnra ons coummnasmres f uid HWHAMHHHNERHEH Hadek maresnrnmunes snentureessous nnavonnomor uen wrofe ap Oorioyimirmamenmer smmrinigonatem emteviecs neuntharon Soomnttansionmore MWtmsfi d messmmenmtwine — 3 r tm rtomanedar commimeermarcnmes M,T..... nmorsinans sn reies | | Anemicanctooy inihranees e io Anounotre | miuume nuomsto towe cett rapon mc mnmmamrmie e ——= sn w Aarctonc hm | Antrmm [ hm wmm ho aniesmms ntm meonuy oob trame mssn ie es esmm rer emineinemsonnonerer bmpetries Gomreaien m sw mrmen [ mnioiorem se nmanmoa‘e Ges: hecmaem Tooanme pa‘ssst fenrame s mromois ‘s! Glsat Monthly Progress Report 01204 Pusersn Page? LORAL

Celsat Action hems Die T m Action Comment Emm _fi es . io rrored ho ueeetreemerncetines 19 tAg Incease#Focolements +008 mprovement. Sconfouraton and accommodaton needs n process i122t sns it ies > , ez >> mt | +o Usentgrated antena temporatire on a beam 200now used. Intogrted eaemp over antemna FOV should Inprocess 3| zng mpoen > |"i—kug. |"In—hoam and beanroam inoerense inclonaf Risen,frowe, To t ordereduang Rivercamr haps: Reduand carier capaoly n process ‘ Pooims. can b compensated by increasingreuseforltsstom. Txg Immpmmamnemimaen uo memas romes k COWA inoface requremont . tAg What is max fcodesicaria possbla? a ¥A9 Gateway archtactre. Prosenappronch detroctos al spectum Alomateapproach coud mprove sstom portamance by minmizng i process mds imiegenninnt amim begimen. appbportinentecnenn romied Aoom, fora satoffoadstoa given GW for pocessing. Atorata mutile paths fo prase cotrl. Aso, ul alow tme phased Increases sis design— moactlo se accommodationTBD cooespaiien eireeresntt Tson iige in s tAg 2 covcated sateites using coherent 2 apertrespace comoring Does M use 2 Tx antemnas t avad mutiacton and space Cosed 8| 10—Aig Meansofredicng e downinkbandvidh and nurmibe of Comonsen on in ies Curent dosignalous ful 2:20 Mz pofond wmont. Tunatio C in process i o naeikgeine Firs? Gan we atccate S—band bandvich tous fooden . , I— m rearppmaummens sutoret muax cone e 8| 10.Au9 |—Refornce mass buigets Suppi eforence mass busget Cosed o 10u9|_Relernce Pover Busgots Suppy reterence power buignt coses S 10 1009 Qualfcaton tatusfor 12mantomnas Same ralacio ason NBSAT Gowd Seee n en Celsat Morthly Progress Report 12104 LORAL e en

Celsat Monthly Progress Report For October 10, 2004 a. Major Program Events: * Submitted new design based on single S—band receive polarization approach. Assumes userterminals are circularly polarized and system does not use polarization diversity combining. New architecture reduces number of gateways from 3 to 2 which reduces overall system cost and potentially improves beamforming control. * Received ROM cost and schedules from 12m antenna suppliers.. Evaluating costisi/schedule. * Initited generation ofrepeater equipment mini—specifications to begin detailed design work ofcritical equipment items. Held status review meeting with Celsat on 21 September. A Product Assurance Program Manager is being assigned to oversee product assurance implementation per Exhibit C. Exhibit C, Product Assurance Program Plan, will verify facilities, parts, processes, procedures and personnel are appropriate and qualified for the Celsat satelite construction. SSAL‘s quality system is fully documented, and is available t all employees on—line through the company intranct. The quality system addresses the life eycle of SS/.‘s products from development through engineering, tst, unit and component manufacturing, subsystem integration, and satellite assembly, integration and test (AIT), and launch. b. Technical Status: 1. Spacceraft — See attached description for current design status summary.. Basic spacceraft design is unchanged from previous report. Minor modifications for new repeater design accounted for. — Initil spacecraft assessment of modified payload design completed. — Updated mass, power, thermal, propellant analyses to incorporate modified payload design.— Results show spacecraft is within normal design limits for satellite and launch vehicles. —— Propellant analyses continues to show positive mass margin after incorporation of payload modifications. —— Interfacing of spacecraf to candidate 4m fairing compatible launch vehicles is being evaluated —— Continuing to work closely with potential antenna suppliers to define initil stowage and deployment interface requirements. Source selection to be made in the next few months — Attitude control group evaluating inclined orbit operation and spacecraft requirement to fly 20—30 degrees offearth—pointing normal to obtain FOV and optimum antenna configuration. The incorporation of pointing control mechanism being evaluated. 2.. Payload — The payload detailed design is undervay. Antenna design is unchanged from previous report. Repeater equipment is updated for new design. Gelsat Monthl Progress Repot 10/10/04 "Aaar Page 1 LORAL

— Assessment of payload modifications for new design completed and incorporated in revised prelimary layout. — Redundancy for critical repeater units added since "gracefil" degradation from multiple pathways not possible since only single polarization pathway is implemented. 6 sets of 10:8 S—band TWTAs, 12 sets of 5:4 S—band LNAs for CONUS beams, 1 set of 4:2 S—band LNAs for HI and PR, 16 sets of 4:3 S—Ka upconverters for CONUS and 2 sets of2:1 S—Ka upconverters for HI and PR. (see block diagram). — Selection of payload load unit designs has begun. — Analysis of 12m unfurlable antenna with 48 element array for CONUS and AK is in progress. Separate subarrays provide HI and PR/USVcoverage.. Finalization ofantenna design based on coverage area, performance, repeater equipment factor, and configuration and C/I will be completed over the next month. No changes are being made to the design which incorporates 46 clements for transmit and 48 elements for receive. Transmit and receive are being individually optimized. Continuing S—band antenna peformance trades between G/T, EIRP and C/L. Evaluation of different beam sizes for 0.35 and 0.5 degree spacings have been added to the optimizations for various scenarios offrequency reuse for capacity including K = 3 thru 12 cases. These are currently in process. —— Baseline repeater channelization initilly unchanged: provides full 20MHz MSS band to support ground—based beamforming architecture using analog S—band channel filtrs. Since actual Celsat frequency allocation has not been determined, an analsis is being performed to determine the impact of a tunable filer to replace fixed 20 MHz bandwidth units.. This would enable the satellite to tune to one or more segments of the MSS spectrum once the final allocations are determined by the FCC. Currently 4 to 5 Mz per system is expected to be allocated. —— In process of generating proposal for further investigation into calibration and pointing coefficient methodology to support ground—base beamforming. Detailed repeater equipment lst being refined. Discussions with suppliers started. 3.. Bus—— The bus detailed design is underway. Bus subsystems are unchanged from previous report. Layout is modified for new repeater equipment items. — The current iPStar—type bus structure is expected to support the modified payload design. Main area ofchange on communications panel layouts. — Initil layout and configuration studies for new design started. Routing for redundancy requires additional layout time. Optimizing comm panel layout for payload performance. — No change to propulsion and station—keeping strategy caused by modified payload. — No change to electrical power design caused by modified payload. —— Evaluating TT&C on—station command pathways for 2 gateway architecture used by modified payload. —— In discussions with vendors to procure common bus components not presently in inventory. c.. Program Controls: Glsat Monthy Progross Report 1/10004 ‘Aaar Page2 LORAL

1. Schedule — Program schedule attached. Current program chedule still supports FCC filing date to bring frequencies into use by Feb 17, 2007, Schedule driver will be 12m antenna subsystem including reflector and boom. Unfurlable antenna system is on critial path. Schedule will be updated upon evaluation of antenna supplier proposals. Mitigation plan to be submitted based on schedule impacts. 2.. Major NCR Status—None. 3. Class 1 Waivers, Deviations — None. 4.. Status oOutstanding Action Items — See attached. 5.. Invoice Status — No outstanding invoices. Received Milestone Payment No. 6. 6.. Status ofContract Changes — None. Gelsat Monthly Progross Repot 1010/04 Ehnar Page 3 LORAL

Celsat Spacecraft Key Features Chamatzaton zoune Stand Artenna Retecr 12im untatatie Admngten ene Feod 4b lomont aray ++ PR Karband Aetomna Reteci 2mige reod 2 spotends wen Sm soe asw nor twra Katans sa csw sos mm Mass sitie DC Pover solum ThomalDsspaton 3.tkw ‘noe rernaCommmynon Pratem sen 1s00 Oy mass 2sSig 12mRatoco: Sevice io 12yous Electcal Power 00 Power anmweo. soirArays 281 +2 Gate panls parwing Batetes 2 3zc0t 170. NH botores Prepuon Bpropetont 2140 k storge tak, 12 20GS twustos, MST Data Harang 56. Omene Suportud seraltus ABuce Gonve #atenl, iBimeAng—Laser Gyros, eath and sun sersors Statontooping +—8degNo Thoma! Raddato pandlsheatopes, htors Nantals, aptcalrafactors Mactorioms 2 ouraray drve assenties Tec Chand oritraiing. Kaband onataton,commant encypton Launctvenices im Proign, Sealaaech), on (Pane5, Atas$, H2A) Celsat Monthy Progress Report 10/1004 Page d

Payload Block Diagram ananten )47 «pemnerrus tB4 worn Coist Bc Dagam Snge RET Po nev aorsioe Celsat Monthy Progress Report 10ri0s poanmpnorm Pages LORAL

n a Imta mooe 4 len Imxroaa nor um un preri hermetiencin un uie nan ma rmmmmce m Mrow sorve monior in Strhain intaties on f Runipinince enountiater s4 lt o mm inetaignent an natiees uesn in onbmmm.com RMuraime th i ‘in aal an fumalon asr on i tm es qoiz isae on w Rmmaciee e lan t dpeeon azm un on i4 Rnoour Ieaake a i9 Mrarce & f In ssm & f hrwnntinadon fa Wtc omcs has «n a0 Iemitoona & monnigrmnniny a lout m im mege zs mtrormn ar—an mtroamanm o vak In tr mamycows us oi prn w ‘an dn innommngme m——fe ie wirge m ns is Primary G/T Summary Gelsa Morthly Progress Repot 101004 snacemerem Page 6

ramanisecontan comge fexest fevace s iwt ‘a S *4 on uie e s0% 12% ie Reoer ie ce oe uo 12% nnafnes o in se m 12% 12% [ en eomemes se MA**8 emanpiae <um Innonantra ermrers nsl [mamaionanar se belatn essune Nok xm ——* % a& (is e m esols #i Punoemnt it f omemvenes x fmona femed omarnyan fconos ts cavana s 4: ‘% 8& ce ue4 s 5 i. :# lots meuaror meronmecuts romnen fnamony hnd in ains a : 2 # caen rne o 4 # & froce 4#_# Spacecraft Mass Budget Mass Risk S to to x Structure a991] 349 70% Mechanisms 18.7 os 18% Propulsion 145.5 s2 s6% Electrical Power ssao| 120 36% Solar Array 1709 ss 40% RepeaterTransponder soas| se4 10.0% Communications Antenna 2020| 203 10.0% Trac 156 o8 s0% apcs T30 15 20% Data Handling System se.r s1 35% Thermal Control 1901| is9 70% Electrical Integration 130.0 o2 _70% Spacecraft—Dry Nominal 2e7 Spacecraft—Dry wl Risk Spaccerat Power Budget Celsat Monthy Progress Report 10/10/04 Page 7 LORAL

Electieal Power (Watts [sussverem "munoe utsee Paycas w ons i73 mc sas ocs toad Propusion sal lers 1se9 (ema! sana bomoss ars svesverarront mara Batey Crarinarcnarymg toss wos oischarger toss kow—valtage Commrter Losses laten—2CU Hamess toss sraceomiet rorat Soor Aray Capmonty (@ EO1¥ y) tA Shadoning Losses Botr Aray Capabity (Shadowing incuded) lsouar array no—racure uaron S raiure Contngoncy(1 erer Greut) [ssAray Gapabity (E0L wth Shadoningrra Isouar array worsr—case mrom [natie Batey Fover worst—case satrery 000 Batt Gat Faiure Contngency (e cets) (worst.case satrery non Celsat Monthy Progress Report trrorne Page s LORAL

Propram Schedule Colsat Program MasterSchedule vessuies mrornrancamrora | ncommnmronsmnere « he4 fln l e 452 n urmnremense | |_onentunensson mnsomcnmonen — | wneor | contentesmmrsone Soamommzeseateen ontasine Sncenttnstznenm on sersmmumnstvare Grmtoow ccrmrsooernsm m Aominenatoon Anerstore sw ooe armran |remmmennseoune ttrranternis snoancorntritor s rrosinsiomemonpremy mm rrovintey ormurenoncancommoncarr ints compean ow = navene Iomaa) mnntoyrmenmy Wwrimeaetes Onerrer nnerstuitin | memessater Celsat Monthy Progross Report 107104 Page 0 LORAL

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