Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20051014-00200 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2005101400200_459779

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: 4 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: 216 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) 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 Parts of southern CONUS to -8 dB rel. gain contour (see GXT file) SA2 S B (Brazil) SA3 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) MKR R 33.8 25 0.15 1 27 N 0 SA1 590 6.1 -99 18 1 MKR R 33.8 25 0.15 1 27 N 90 SA1 590 6.1 -99 18 1 MKT T 32.6 24.7 0.15 1 27 N 0 SA1 1.9 18.8 51.4 MKT T 32.6 24.7 0.15 1 27 N 90 SA1 1.9 18.8 51.4 BRR R 33.8 25.4 0.15 1 27 N 0 SA2 620 5.9 -99 18 1 BRR R 33.8 25.4 0.15 1 27 N 90 SA2 620 5.9 -99 18 1 BRT T 32.5 24.7 0.15 1 27 N 0 SA2 1.9 18.8 51.3 BRT T 32.5 24.7 0.15 1 27 N 90 SA2 1.9 18.8 51.3 GBL T 19.6 16.6 0.15 1 30 N 0 SA3 4 0.088 9 GBL T 19.6 16.6 0.15 1 30 N 90 SA3 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) MKR R C -70 MMKRH.GXT MKR R C -70 MMKRV.GXT MKT T C -70 MMKTH.GXT -157.9 -156.8 -155.6 -154.5 -153.4 MKT T C -70 MMKTV.GXT -157.9 -156.8 -155.6 -154.5 -153.4 BRR R C -70 BRR R C -70 BRT T C -70 -159.9 -159.8 -159.6 -159.5 -159.4 BRT T C -70 -159.9 -159.8 -159.6 -159.5 -159.4 GBL T C -70 GBLH.gxt -153 -153 -153 -153 -153 GBL T C -70 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) KU001 36000 R 14040 V C TK001 128.6 KU001 MKRV KD001 BRTH KU002 72000 R 14180 V C TK002 128.6 KU001 BRRV KD001 MKTH KU003 72000 R 14320 H C TK003 128.6 KU002 MKRV KD002 BRTH KU004 36000 R 14460 H C TK004 128.6 KU002 BRRV KD002 MKTH KD001 36000 T 11740 H C TK005 128.6 KU003 MKRH KD003 BRTV KD002 72000 T 11880 H C TK006 128.6 KU003 BRRH KD003 MKTV KD003 72000 T 12020 V C TK007 128.6 KU004 MKRH KD004 BRTV KD004 36000 T 12160 V C TK008 128.6 KU004 BRRH KD004 MKTV BN01 25 T 11700.5 H T BN01 BN01 GBLH BN02 25 T 12199.3 V T BN02 BN02 GBLV

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

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 25K0N0N 25 7 9.2

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) TK001 TK008 D05 96 750 K3 LB.doc 46.6 7.4 15.4 19.5 26.5 -157 30.9 TK001 TK008 D05 55 750 K4 LB.doc 54.5 3 11 24 30 -153 22.9 TK001 TK008 D04 30 1975 K5 LB.doc 49.1 10.9 18.9 26.5 32.5 -155 33.4 TK001 TK008 D04 18 1975 K6 LB.doc 57 6 13 30 35 -153 25.4 TK001 TK008 D03 10 6875 K7 LB.doc 57 9 15 31 37 -156 33.4 TK001 TK008 D02 4 18000 K8 LB.doc 59 10.5 17.5 37 41 -157 35.3 TK001 TK008 D01 1 K9 LB.doc 59 16 24 42 50 -151 22.9 BN01 BN02 A01 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): #Error

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): 6488 6488 6488 6488 Bus (Watts): (b): (g): (l): (q): 1962 1550 1962 1550 Total (Watts): (c): (h): (m): (r): 8450 8038 8450 8038 Solar Array (Watts): (d): (i): (n): (s): 9707 9020 8825 8200 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: 2005-10-17 12:07:33
Document Modified: 2005-10-17 12:07:33
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC