Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20050706-00143 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2005070600143_440278

FCC 312 FEDERAL COMMUNICATIONS COMMISSION Page 1: General, Schedule S SATELLITE SPACE STATION AUTHORIZATIONS Frequency Bands, (Technical and Operational Description) and GSO Orbit S1. GENERAL INFORMATION Complete for all satellite applications. a. Space Station or Satellite Network Name: e. Estimated Date of Placement into Service: i Will the space station(s) operate on a Common Carrier Basis: STAR ONE C1 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 42 0 MHz d1. Est Launch Date Begin: d2. Est Launch Date End: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply: 1581 MHz GSO NGSO X S2. OPERATING FREQUENCY BANDS Identify the frequency range and transmit/receive mode for all frequency bands in which this station will oper Also indicate the nature of service(s) for each frequency band. Frequency Band Limits Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode f. Nature of Service(s): List all that apply to this band a. Numeric b. Unit c. Numeric d. Unit (K/M/G) (K/M/G) 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 11700 M 12200 M T Fixed Satellite Service S3. ORBITAL INFORMATION FOR GEOSTATIONARY SATELLITES ONLY: a. Nominal Orbital Longitude (Degrees E/W): b. Alternate Orbital Longitude (Degrees E/W): c. Reason for orbital location selection: 65 W The Brazilian telecommunications authority has Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be authorized Star One to operate the STAR ONE C1 N/S Station-Keeping provided (Optional): satellite at 65° W.L. d. Toward West: Degrees E/W 0.05 Degrees Tolerance: g. Westernmost: e. Toward East: 0.05 Degrees 0.1 Degrees h. Easternmost: i. Reason for service are selection (Optional):

FEDERAL COMMUNICATIONS COMMISSION Page 2: NGSO Orbits SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S4. ORBITAL INFORMATION FOR NON-GEOSTATIONARY SATELLITES ONLY S4a. Total Number of Satellites in Network or System: S4c. Celestial Reference Body (Earth, Sun, Moon, etc.): S4b. Total Number of Orbital Planes in Network or System: S4d. Orbit Epoch Date: For each Orbital Plane Provide: (e) Orbital (f) No. of (g) Inclination (h) Orbital (i) Apogee (km) (j) Perigee (km) (k) Right Ascension (l) Argument of Active Service Arc Range (Degrees) Plane No. Satellites in Angle (degrees) Period of the Ascending Perigee (m) Begin (n) End (o) Other Plane (Seconds) Node (Deg.) (Degrees) Angle Angle S5. INITIAL SATELLITE PHASE ANGLE For each satellite in each orbital plane, provide the intital phase angle. (a) Orbital (b) Satellite (c) Initial Plane No. Number Phase Angle (Degrees) NO NGSO DATA FILED

FEDERAL COMMUNICATIONS COMMISSION Page 3: Service Areas SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S6. SERVICE AREA CHARACTERISTICS for each service area provide: (a) Service Area (b) Type of Associated (c) Service Area Diagram (d) Service Area Description. Provide list of geographic areas (state postal codes or ITU 3-ltr codes), satellites or Figure No. of ID Station (Earth or File Name (GXT File) Service Area Diagram. Space) SA1 S South America, Central America, Mexico, USA SA2 S South America, Central America, Mexico, USA SA3 S Brazil SA4 S South America, USA SA5 S Region 2

FEDERAL COMMUNICATIONS COMMISSION Page 4: Antenna Beams SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S7. SPACE STATION ANTENNA BEAM CHARACTERISTICS For each antenna beam provide: (a) (b) Isotropic Antenna (e) (f) (g) Min. (h) Polar- (i) Polarization (j) Service Transmit Receive Beam T/R Gain Pointing Rotational Cross- ization Alignment Rel. Area ID (k) (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Input Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) Losses Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) (db/K) (dBW/m2) BSC R 29.7 19.7 0.09 0.02 27 N 0 SA1 617 1.8 -96.8 18 0.5 BSC R 29.7 19.7 0.09 0.02 27 N 90 SA1 617 1.8 -96.8 18 0.5 BSC T 26.2 16.2 0.09 0.02 27 N 0 SA1 2.9 28.2 40.7 BSC T 26.2 16.2 0.09 0.02 27 N 90 SA1 2.9 28.2 40.7 BKR R 34 26 0.09 0.02 28 N 90 SA3 660 5.8 -98.8 18 1 BKR R 34 26 0.09 0.02 28 N 0 SA3 660 5.8 -98.8 18 1 MKR R 32.2 24.2 0.09 0.02 28 N 90 SA4 668 4 -97 18 1 MKR R 32.2 24.2 0.09 0.02 28 N 0 SA4 668 4 -97 18 1 BKTV T 32 24 0.09 0.02 28 N 90 SA3 2.3 68.9 50.4 BKT T 32 24 0.09 0.02 28 N 0 SA3 2.3 68.9 50.4 MKT T 31.6 23.6 0.09 0.02 28 N 90 SA4 2.3 68.9 50 MKT T 31.6 23.6 0.09 0.02 28 N 0 SA4 2.3 68.9 50 GBL T 19.6 16.6 0.09 0.02 30 N 0 SA5 4 0.088 9 GBL T 19.6 16.6 0.09 0.02 30 N 90 SA5 4 0.088 9

FEDERAL COMMUNICATIONS COMMISSION Page 5: Beam Diagrams SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S8. ANTENNA BEAM DIAGRAMS For each beam pattern provide the reference to the graphic image and numerical data: Also provide the power flux density levels in each beam that result from the emission with the highest power flux density. (a) (b) (c) Co-or (d) GSO (e) NGSO Antenna Gain (f) GSO Antenna Max. Power Flux Density (dBW/M2/Hz) Beam T/R Cross Ref. Contour Description Gain Contour Data At Angle of Arrival above horizontal (for emission with highest PFD) ID Mode Polar Orbital (Figure/Table/ Exhibit) (GXT File) (g) 5 Deg (h) 10 Deg (i) 15 Deg (j) 20 Deg (k) 25 Deg Mode ("C" Longitude or" X") (Deg. E/W) BSC R C -65 BSCRH.GXT BSC R C -65 BSCRV.GXT BSC T C -65 BSCTH.GXT -157.5 -157.3 -156.8 -155.4 -154.6 BSC T C -65 BSCTV.GXT -157.5 -157.3 -156.8 -155.4 -154.6 BKR R C -65 BKRV.GXT BKR R C -65 BKRH.GXT MKR R C -65 MKRV.GXT MKR R C -65 MKRH.GXT BKTV T C -65 BKTV.GXT -161.2 -160.9 -160.7 -160.6 -155.5 BKT T C -65 BKTH.GXT -161.2 -160.9 -160.7 -160.6 -155.5 MKT T C -65 MKTV.GXT -157.1 -155.2 -153.5 -151.4 -148.8 MKT T C -65 MKTH.GXT -157.1 -155.2 -153.5 -151.4 -148.8 GBL T C -65 GBLH.gxt -153 -153 -153 -153 -153 GBL T C -65 GBLV.gxt -153 -153 -153 -153 -153

FEDERAL COMMUNICATIONS COMMISSION Page 6: Channels and SATELLITE SPACE STATION AUTHORIZATIONS Transponders FCC Form 312 - Schedule S: (Technical and Operational Description) S9. SPACE STATION CHANNELS For each frequency channel provide: S10. SPACE STATION TRANSPONDERS For each transponder provide: (a) (B) Assigned (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band Channel Bandwidth T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID No. (kHz) Mode (MHz) (H, V, L, R) Channel ID Gain (dB) No. ID No. (T or C) CU001 36000 R 5925 H C TC001 119.2 CU001 BSCRH CD001 BSCTV CU003 36000 R 5965 H C TC003 119.2 CU003 BSCRH CD003 BSCTV CU005 36000 R 6005 H C TC005 119.2 CU005 BSCRH CD005 BSCTV CU007 36000 R 6045 H C TC007 119.2 CU007 BSCRH CD007 BSCTV CU009 36000 R 6085 H C TC009 119.2 CU009 BSCRH CD009 BSCTV CU011 36000 R 6125 H C TC011 119.2 CU011 BSCRH CD011 BSCTV CU013 36000 R 6165 H C TC013 119.2 CU013 BSCRH CD013 BSCTV CU015 36000 R 6205 H C TC015 119.2 CU015 BSCRH CD015 BSCTV CU017 36000 R 6245 H C TC017 119.2 CU017 BSCRH CD017 BSCTV CU019 36000 R 6285 H C TC019 119.2 CU019 BSCRH CD019 BSCTV CU021 36000 R 6325 H C TC021 119.2 CU021 BSCRH CD021 BSCTV CU023 36000 R 6365 H C TC023 119.2 CU023 BSCRH CD023 BSCTV CU025 36000 R 6405 H C TC025 119.2 CU025 BSCRH CD025 BSCTV CU002 36000 R 5945 V C TC002 119.2 CU002 BSCRV CD002 BSCTH CU004 36000 R 5985 V C TC004 119.2 CU004 BSCRV CD004 BSCTH CU006 36000 R 6025 V C TC006 119.2 CU006 BSCRV CD006 BSCTH CU008 36000 R 6065 V C TC008 119.2 CU008 BSCRV CD008 BSCTH CU010 36000 R 6105 V C TC010 119.2 CU010 BSCRV CD010 BSCTH CU012 36000 R 6145 V C TC012 119.2 CU012 BSCRV CD012 BSCTH CU014 36000 R 6185 V C TC014 119.2 CU014 BSCRV CD014 BSCTH CU016 36000 R 6225 V C TC016 119.2 CU016 BSCRV CD016 BSCTH CU018 36000 R 6265 V C TC018 119.2 CU018 BSCRV CD018 BSCTH CU020 36000 R 6305 V C TC020 119.2 CU020 BSCRV CD020 BSCTH CU022 36000 R 6345 V C TC022 119.2 CU022 BSCRV CD022 BSCTH CU024 36000 R 6385 V C TC024 119.2 CU024 BSCRV CD024 BSCTH CD001 36000 T 3700 V C TK001 127.8 KU001 MKRV KD001 MKTH CD003 36000 T 3740 V C TK002 127.8 KU001 MKRV KD001 BKTH CD005 36000 T 3780 V C TK003 127.8 KU001 BKRV KD001 MKTH CD007 36000 T 3820 V C TK004 127.8 KU002 MKRV KD002 MKTH CD009 36000 T 3860 V C TK005 127.8 KU002 BKRV KD002 BKTH

CD011 36000 T 3900 V C TK006 127.8 KU002 MKRV KD002 BKTH CD013 36000 T 3940 V C TK007 127.8 KU003 MKRH KD003 MKTV CD015 36000 T 3980 V C TK008 127.8 KU003 MKRH KD003 BKTV CD017 36000 T 4020 V C TK009 127.8 KU003 BKRH KD003 MKTV CD019 36000 T 4060 V C TK010 127.8 KU004 MKRH KD004 MKTV CD021 36000 T 4100 V C TK011 127.8 KU004 MKRH KD004 BKTV CD023 36000 T 4140 V C TK012 127.8 KU004 BKRH KD004 MKTV CD025 36000 T 4180 V C CM01 CMD01 BSCRV CD002 36000 T 3720 H C CM02 CMD02 BSCRH CD004 36000 T 3760 H C TM01 TLM01 BSCTH CD006 36000 T 3800 H C TM02 TLM02 BSCTH CD008 36000 T 3840 H C BN01 BN01 GBLH CD010 36000 T 3880 H C BN02 BN02 GBLV CD012 36000 T 3920 H C CD014 36000 T 3960 H C CD016 36000 T 4000 H C CD018 36000 T 4040 H C CD020 36000 T 4080 H C CD022 36000 T 4120 H C CD024 36000 T 4160 H C KU001 36000 R 14040 V C KU002 72000 R 14180 V C KU003 72000 R 14320 H C KU004 36000 R 14460 H C KD001 36000 T 11740 H C KD002 72000 T 11880 H C KD003 72000 T 12020 V C KD004 36000 T 12160 V C CMD01 820 R 6424.5 V T CMD02 820 R 6424.5 H T TLM01 200 T 4199 H T TLM02 200 T 4199.9 H T BN01 25 T 11701 H T BN02 25 T 12199.8 V T

FEDERAL COMMUNICATIONS COMMISSION Page 7: Digital Modulation SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S11. DIGITAL MODULATION PARAMETERS For each digital emission provide: (a) Digital (b) Emission (c) Assigned (d) No. of (e)Uncoded (f) FEC Error (g) CDMA (h) Total C/N (i) Single Entry Mod. ID Designator Bandwidth Phases Data Rate Correction Processing Performance C/I Objective (kHz) (kbps) Coding Rate Gain (dB) Objective (dB) (dB) D01 36M0G7W 36000 4 48400 0.806 7.8 20 D02 17M9G7W 17900 8 34368 0.768 12.4 24.6 D03 5M50G7W 5500 8 8448 0.614 9.4 21.6 D04 1M64G7W 1640 4 2048 0.75 8.5 20.7 D05 614KG7W 614 4 512 0.5 5.7 17.9 D06 5K80G7W 5.8 4 4.8 0.5 5.7 17.9

FEDERAL COMMUNICATIONS COMMISSION Page 8: Analog Modulation SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S12. ANALOG MODULATION PARAMETERS For each analog emission provide: (a) (b) Emission (c) (d) Signal (e) Multi-channel Telephony (j) Video (k) Video (l) Video (m) SCPC/FM (n) Total C/N (o) Single Analog Designator Assigned Type Channels Standard Noise- and Compander, Performance Entry C/I (f) Ave. (g) Bottom (h) Top (i) RMS Mod. ID Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective Companded Baseband Baseband Modulation (kHz) PAL, etc. (dB) Modulation and Noise (dB) (dB) Talker Level Freq. (MHz) Freq. (MHz) Index Index Weighting (dB) (dBm0) A01 17M5F3F 17500 TV/FM NTSC 12.8 1.4 9 23 A02 25M0F3F 25000 TV/FM NTSC 12.8 2 12.5 26.5 A03 820KF2D 820 10 22.2 A04 200KG2D 200 7.5 19.7 A05 25K0N0N 25 7 19.2

FEDERAL COMMUNICATIONS COMMISSION Page 9: Typical Emissions SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S13. TYPICAL EMISSIONS For each planned type of emission provide: Associated Modulation ID (e) Carriers (f) Carrier (g)Noise Budget (h) Energy Receive Band (Assoc. Transmit Stn) Transmit Band (This Space Station) Transponder ID Range per Spacing Reference (Table Dispersal (c) Digital (d) Analog (i)Assoc. Assoc. Station Transmit EIRP (dBW) (n) Max. (o)Assoc. Transponder (kHz) No.) Bandwidth (Table (Table S12) Stn. Max. Power (dBW) Power Flux Stn (a) Start (b) End (kHz) S11) Antenna Density Rec. G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dBW/m2/Hz) (dB/K) TC001 TC024 D06 500 9 C1 LB.doc 39.2 -11.8 -5.2 -7.5 -3.5 -167 24.1 TC001 TC024 D06 500 9 C2 LB.doc 47.2 -12.8 -6.2 0 4 -159 16.2 TC001 TC024 D05 48 750 C3 LB.doc 39.2 8.2 14.8 13 17 -167 24.1 TC001 TC024 D05 48 750 C4 LB.doc 47.2 7.7 14.3 20 24 -160 16.2 TC001 TC024 D04 18 1975 C5 LB.doc 45.2 7.7 14.3 18 22 -166 26.6 TC001 TC024 D04 13 1975 C6 LB.doc 49.7 6.2 12.8 21.5 25.5 -162 22.2 TC001 TC024 D03 5 6875 C7 LB.doc 51.6 6.8 13.4 23.5 27.5 -166 28.6 TC001 TC024 D02 2 18000 C8 LB.doc 53.2 12.2 18.8 29 33 -165 30.1 TC001 TC024 D01 1 C9 LB.doc 53.2 16.7 23.3 36.7 40.7 -161 20.6 TC001 TC024 A01 2 C10 LB.doc 49.7 15.2 21.8 33 36 -153 24.1 TC001 TC024 A02 1 C11 LB.doc 51.6 18.3 24.9 37.7 40.7 -148 16.2 TK001 TK012 D06 500 9 K1 LB.doc 43.1 -7.6 -1.1 2.5 6.5 -157 29 TK001 TK012 D06 500 9 K2 LB.doc 52.6 -9.1 -2.6 11 15 -148 19.4 TK001 TK012 D05 48 750 K3 LB.doc 46.6 8.9 15.4 22.5 26.5 -157 30.9 TK001 TK012 D05 48 750 K4 LB.doc 54.5 4.5 11 26 30 -154 22.9 TK001 TK012 D04 18 1975 K5 LB.doc 49.1 12.4 18.9 28.5 32.5 -155 33.4 TK001 TK012 D04 13 1975 K6 LB.doc 57 4.5 11 31 35 -153 25.4 TK001 TK012 D03 5 6875 K7 LB.doc 57 6.5 13 33 37 -156 33.4 TK001 TK012 D02 2 18000 K8 LB.doc 59 9 15.5 37 41 -155 35.3 TK001 TK012 D01 1 K9 LB.doc 59 15.5 22 46 50 -151 22.9 TK001 TK012 A01 2 K10 LB.doc 57 11 17.5 42 45 -140 27.4 TK001 TK012 A02 1 K11 LB.doc 57 17.5 24 46 49 -140 21.4 CM01 CM02 A03 1 CMD LB.doc 53.2 10.8 15.8 TM01 TM02 A04 1 TLM LB.doc 11 18 -148 27.9 BN01 BN02 A05 1 BCN LB.doc 6 9 -153 29.4

FEDERAL COMMUNICATIONS COMMISSION Page 10: TT and C SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S14. Is the space station(s) controlled and monitored remotely? If Yes, provide the location and telephone number of the TT and C control point(s): Yes

FEDERAL COMMUNICATIONS COMMISSION Page 11: SATELLITE SPACE STATION AUTHORIZATIONS Characteristics and FCC Form 312 - Schedule S: (Technical and Operational Description) Certifications S15. SPACECRAFT PHYSICAL CHARACTERISTICS: S15a: Mass of spacecraft without fuel (kg): Spacecraft Dimensions Probability of Survival to 1812 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2286 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4098 37 0.72 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 800 7.5 0.83 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 65 6.1 0.6 S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: Spacecraft Electrical Power (Watts) At Electrical Power (Watts) At Subsystem Beginning of Life End of Life At Equinox At Solstice At Equinox At Solstice Payload (Watts): (a): (f): (k): (p): 5830 5830 5830 5830 Bus (Watts): (b): (g): (l): (q): 1696 769 1696 769 Total (Watts): (c): (h): (m): (r): 7526 6599 7526 6599 Solar Array (Watts): (d): (i): (n): (s): 10420 9330 8250 7580 Depth of Battery (e) (j) (o) (t) Discharge (%): 75 % 75 % 75 % 75 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: X YES NO N/A b. Are the appropriate service area coverage requirements of § 25.143(b)(ii) and (iii), or § 25.145(c)(1) and (2) met? YES NO X N/A c. Are the frequency tolerances of § 25.202(e) and the out-of-band emission limits of § 25.202(f)(1), (2) and (3) met? X YES NO N/A In addition to the information required in this Form, the space station applicant is required to provide all the information specified in Section 25.114 of the Commission's rules, 47 C.F.R § 25.114.


Document Created: 2005-07-07 13:39:18
Document Modified: 2005-07-07 13:39:18
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