Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20050708-00144 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2005070800144_441411

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 C2 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: 29 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: 1728 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: 70 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 C2 N/S Station-Keeping provided (Optional): satellite at 70° 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 Brazil, Argentina, Uruguay, Chile, USA SA5 S RG2

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 0.9 0.02 27 N 0 SA1 617 1.8 -95 18 0.5 BSC R 29.7 19.7 0.9 0.02 27 N 90 SA1 617 1.8 -95 18 0.5 BSC T 26.2 16.2 0.9 0.02 27 N 0 SA2 2.9 28.2 40.7 BSC T 26.2 16.2 0.9 0.02 27 N 90 SA2 2.9 28.2 40.7 BKR R 32.2 24.1 0.9 0.02 28 N 90 SA3 668 4 -93 18 1 MKR R 32.2 24.2 0.9 0.02 28 N 90 SA4 668 4 -93 18 1 BKT T 31.6 23.6 0.9 0.02 28 N 0 SA3 2.3 68.9 50 MKT T 31.6 23.6 0.9 0.02 28 N 0 SA4 2.3 68.9 50 GBL T 19.6 16.6 0.9 0.02 30 N 0 SA5 4 0.088 9 GBL T 19.6 16.6 0.9 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 -70 BSCRH.GXT BSC R C -70 BSCRV.GXT BSC T C -70 BSCTH.GXT -157 -157 -157 -155 -153 BSC T C -70 BSCTV.GXT -157 -157 -157 -155 -153 BKR R C -70 BKRV.GXT MKR R C -70 MKRV.GXT BKT T C -70 BKTH.GXT -161 -161 -161 -155 -155 MKT T C -70 MKTH.GXT -154 -154 -153 -150 -148 GBL T C -70 GBLH.GXT -157 -157 -157 -156 -156 GBL T C -70 GBLV.GXT -157 -157 -157 -156 -156

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 72000 R 5905 H C TC001 120 CU001 BSCRH CD001 BSCTV CU002 36000 R 5965 H C TC002 120 CU002 BSCRH CD002 BSCTV CU003 72000 R 5965 V C TC003 120 CU004 BSCRH CD004 BSCTV CU004 36000 R 6005 H C TC004 120 CU006 BSCRH CD006 BSCTV CU005 36000 R 6025 V C TC005 120 CU008 BSCRH CD008 BSCTV CU006 72000 R 6065 H C TC006 120 CU010 BSCRH CD010 BSCTV CU007 36000 R 6065 V C TC007 120 CU012 BSCRH CD012 BSCTV CU008 36000 R 6125 H C TC008 120 CU014 BSCRH CD014 BSCTV CU009 72000 R 6125 V C TC009 120 CU016 BSCRH CD016 BSCTV CU010 36000 R 6165 H C TC010 120 CU018 BSCRH CD018 BSCTV CU011 36000 R 6185 V C TC011 120 CU003 BSCRV CD003 BSCTH CU012 36000 R 6205 H C TC012 120 CU005 BSCRV CD005 BSCTH CU013 36000 R 6225 V C TC013 120 CU007 BSCRV CD007 BSCTH CU014 36000 R 6245 H C TC014 120 CU009 BSCRV CD009 BSCTH CU015 72000 R 6285 V C TC015 120 CU011 BSCRV CD011 BSCTH CU016 72000 R 6305 H C TC016 120 CU013 BSCRV CD013 BSCTH CU017 72000 R 6365 V C TC017 120 CU015 BSCRV CD015 BSCTH CU018 72000 R 6385 H C TC018 120 CU017 BSCRV CD017 BSCTH CD001 72000 T 3680 V C TK001 137.5 KU001 MKRV KD001 MKTH CD002 36000 T 3740 V C TK002 137.5 KU002 MKRV KD002 MKTH CD003 72000 T 3740 H C TK003 137.5 KU001 BKRV KD001 MKTH CD004 36000 T 3780 V C TK004 137.5 KU002 BKRV KD002 MKTH CD005 36000 T 3800 H C TK005 137.5 KU001 MKRV KD001 BKTH CD006 72000 T 3840 V C TK006 137.5 KU002 MKRV KD002 BKTH CD007 36000 T 3840 H C CM01 CMD01 BSCRV CD008 36000 T 3900 V C CM02 CMD02 BSCRV CD009 72000 T 3900 H C TM01 TLM01 BSCTH CD010 36000 T 3940 V C TM02 TLM02 BSCTH CD011 36000 T 3960 H C BN01 BN01 GBLH CD012 36000 T 3980 V C BN02 BN02 GBLV

CD013 36000 T 4000 H C CD014 36000 T 4020 V C CD015 72000 T 4060 H C CD016 72000 T 4080 V C CD017 72000 T 4140 H C CD018 72000 T 4160 V C KU001 72000 R 14220 V C KU002 72000 R 14460 V C KD001 72000 T 11920 H C KD002 72000 T 12160 H C CMD01 820 R 6423.6 V T CMD02 820 R 6424.4 V T TLM01 200 T 4199 H T TLM02 200 T 4199.8 H T BN01 25 T 11701 H T BN02 25 T 12199 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 2 NTSC 12.8 1.4 9 23 A02 25M0F3F 25000 TV/FM 1 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 TC018 D01 500 9 C1 LB.doc 39.2 -11.8 -5.2 -7.5 -3.5 -167 24.1 TC001 TC018 D01 500 9 C2 LB.doc 47.2 -12.8 -6.2 0 4 -159 16.2 TC001 TC018 D02 48 750 C3 LB.doc 39.2 8.2 14.8 13 17 -167 24.1 TC001 TC018 D02 48 750 C4 LB.doc 47.2 7.7 14.3 20 24 -160 16.2 TC001 TC018 D03 18 1975 C5 LB.doc 45.2 7.7 14.3 18 22 -166 26.6 TC001 TC018 D03 13 1975 C6 LB.doc 49.7 6.2 12.8 21.5 25.5 -162 22.2 TC001 TC018 D04 5 6875 C7 LB.doc 51.6 6.8 13.4 23.5 27.5 -166 28.6 TC001 TC018 D05 2 18000 C8 LB.doc 53.2 12.2 18.8 29 33 -165 30.1 TC001 TC018 D06 1 C9 LB.doc 53.2 16.7 23.3 36.7 40.7 -161 20.6 TC001 TC018 A01 2 18000 C10 LB.doc 49.7 15.2 21.8 33 36 -153 24.1 TC001 TC018 A02 1 C11 LB.doc 51.6 18.3 24.9 37.7 40.7 -148 16.2 TK001 TK006 D01 500 9 K1 LB.doc 43.1 -7.6 -1.1 2.5 6.5 -157 29 TK001 TK006 D01 500 9 K2 LB.doc 52.6 -9.1 -2.6 11 15 -148 19.4 TK001 TK006 D02 48 750 K3 LB.doc 46.6 8.9 15.4 22.5 26.5 -157 30.9 TK001 TK006 D02 48 750 K4 LB.doc 54.5 4.5 11 26 30 -154 22.9 TK001 TK006 D03 18 1975 K5 LB.doc 49.1 12.4 18.9 28.5 32.5 -155 33.4 TK001 TK006 D03 13 1975 K6 LB.doc 57 4.5 11 31 35 -153 25.4 TK001 TK006 D04 5 6875 K7 LB.doc 57 6.5 13 33 37 -156 33.4 TK001 TK006 D05 2 18000 K8 LB.doc 59 9 15.5 37 41 -155 35.3 TK001 TK006 D06 1 K9 LB.doc 59 15.5 22 46 50 -151 22.9 TK001 TK006 A01 2 18000 K10 LB.doc 57 11 17.5 42 45 -140 27.4 TK001 TK006 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: 1200 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: 2005-07-14 17:38:21
Document Modified: 2005-07-14 17:38:21
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