Attachment Schedule S Tech Data

This document pretains to SAT-LOI-20081119-00217 for Letter of Intent on a Satellite Space Stations filing.

IBFS_SATLOI2008111900217_679876

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: BSSNET103W 12/30/2012 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 6/30/2009 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 10/30/2011 26 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: 12/30/2011 12/30/2011 676 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) 17.3 G 17.7 G T Broadcasting Satellite Service - Data 17.3 G 17.7 G T Broadcasting Satellite Service - Sound 17.3 G 17.7 G T Broadcasting Satellite Service - Video 17.3 G 17.7 G T PTTC 24.75 G 25.15 G R Broadcasting Satellite Service - Data 24.75 G 25.15 G R Broadcasting Satellite Service - Sound 24.75 G 25.15 G R Broadcasting Satellite Service - Video 24.75 G 25.15 G R TTC 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: 103.15 W Available Appendix F offset orbital location Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be N/S Station-Keeping provided (Optional): d. Toward West: Degrees E/W 0.05 Degrees Tolerance: g. Westernmost: e. Toward East: 0.05 Degrees 0.05 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) CONUS+ S USA, HWA, ALS, ATN, PTR, VIR, ABW LAUL S ULLA SA.gxt Spot LA Uplink CMD S SP31R SA.gxt Command from LA TEL S SP31R SA.gxt Telemetry to LA CRBSPOT S ABW, ATN

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) USA T 36.1 21.1 0.15 30 N CONUS+ 1.5 313 61.1 LAUL R 47 46 0.1 30 N LAUL 794 17.5 -109 25 0.5 CMD R 47.7 43.7 0.1 30 N CMD 794 18.7 -109 25 0.5 TEL T 36.1 28.7 0.15 30 N TEL 2 0.05 23.1 CMD R 47.7 46 0.1 30 N CRBSPOT 794 18.7 TELC T 36.1 16.4 0.1 30 N CRBSPOT 2 12.59 47.1

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) USA T C -103.15 103 Conus.gxt -116.3 -116.2 -116 -115.9 -115.8 LAUL R C -103.15 ULLA G.gxt CMD R C -103.15 SP31R.gxt TEL T C -103.15 103 Conus.gxt -140.8 -140.8 -140.8 -140.8 -140.8 CMD R C -103.15 SP51R.gxt TELC T C -103.15 103 Conus.gxt -116.8 -116.8 -116.8 -116.8 -116.8

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) FA001 26000 T 17325 L C NA001 156 GA001 LAUL FA001 USA FA003 26000 T 17354.16 L C NA003 156 GA003 LAUL FA003 USA FA005 26000 T 17383.32 L C NA005 156 GA005 LAUL FA005 USA FA007 26000 T 17412.48 L C NA007 156 GA007 LAUL FA007 USA FA009 26000 T 17441.64 L C NA009 156 GA009 LAUL FA009 USA FA011 26000 T 17470.8 L C NA011 156 GA011 LAUL FA011 USA FA013 26000 T 17499.96 L C NA013 156 GA013 LAUL FA013 USA FA015 26000 T 17529.12 L C NA015 156 GA015 LAUL FA015 USA FA017 26000 T 17558.28 L C NA017 156 GA017 LAUL FA017 USA FA019 26000 T 17587.44 L C NA019 156 GA019 LAUL FA019 USA FA021 26000 T 17616.6 L C NA021 156 GA021 LAUL FA021 USA FA023 26000 T 17645.76 L C NA023 156 GA023 LAUL FA023 USA FA025 26000 T 17674.92 L C NA025 156 GA025 LAUL FA025 USA FB002 26000 T 17325 R C NB002 156 GB002 LAUL FB002 USA FB004 26000 T 17354.16 R C NB004 156 GB004 LAUL FB004 USA FB006 26000 T 17383.32 R C NB006 156 GB006 LAUL FB006 USA FB008 26000 T 17412.48 R C NB008 156 GB008 LAUL FB008 USA FB010 26000 T 17441.64 R C NB010 156 GB010 LAUL FB010 USA FB012 26000 T 17470.8 R C NB012 156 GB012 LAUL FB012 USA FB014 26000 T 17499.96 R C NB014 156 GB014 LAUL FB014 USA FB016 26000 T 17529.12 R C NB016 156 GB016 LAUL FB016 USA FB018 26000 T 17558.28 R C NB018 156 GB018 LAUL FB018 USA FB020 26000 T 17587.44 R C NB020 156 GB020 LAUL FB020 USA FB022 26000 T 17616.6 R C NB022 156 GB022 LAUL FB022 USA FB024 26000 T 17645.76 R C NB024 156 GB024 LAUL FB024 USA FB026 26000 T 17674.92 R C NB026 156 GB026 LAUL FB026 USA GA001 26000 R 24775 R C C1 CMD1 CMD GA003 26000 R 24804.16 R C C2 CMD2 CMD GA005 26000 R 24833.32 R C T1 TLM1 TEL GA007 26000 R 24862.48 R C T2 TLM2 TEL

GA009 26000 R 24891.64 R C C1CRB CMD1 CMDCR GA011 26000 R 24920.8 R C C2CRB CMD2 CMDCR GA013 26000 R 24949.96 R C T1CRB TLM1 TELCR GA015 26000 R 24979.12 R C T2CRB TLM2 TELCR GA017 26000 R 25008.28 R C GA019 26000 R 25037.44 R C GA021 26000 R 25066.6 R C GA023 26000 R 25095.76 R C GA025 26000 R 25124.92 R C GB002 26000 R 24775 L C GB004 26000 R 24804.16 L C GB006 26000 R 24833.32 L C GB008 26000 R 24862.48 L C GB010 26000 R 24891.64 L C GB012 26000 R 24920.8 L C GB014 26000 R 24949.96 L C GB016 26000 R 24979.12 L C GB018 26000 R 25008.28 L C GB020 26000 R 25037.44 L C GB022 26000 R 25066.6 L C GB024 26000 R 25095.76 L C GB026 26000 R 25124.92 L C CMD1 1000 R 24753 R T CMD2 1000 R 24755 R T TLM1 1000 T 17303 R T TLM2 1000 T 17306 R 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) D1 25M8G7W 25800 8 42570 0.67 7.1 20

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) C1 800KF9D 800 40 50 T1 800KF9D 800 10 30

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) NA001 NB026 D1 1 Comm Link Co 67.6 7 13.5 46.1 61.1 -115 16.4 C1 C2 C1 Command Link 64.4 5 24.5 18.7 T1 T2 T1 Telemetry Link 16 23.1 -140.8 41.2 C1CRB C2CRB C1 64.4 5 24.5 18.7 T1CRB T2CRB T1 27.4 47.1 -116.8 41.2

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 Remote Control (TT C) Location(s): S14a: Street Address: S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Curacao S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):

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 3715 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2684 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6399 50 0.6 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 277 8.2 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 80 7.3 0.51 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): 16704 16704 16704 16704 Bus (Watts): (b): (g): (l): (q): 1766 955 1766 955 Total (Watts): (c): (h): (m): (r): 18470 17659 18470 17659 Solar Array (Watts): (d): (i): (n): (s): 23124 20643 20905 19583 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? X YES NO 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: 2008-11-20 12:04:09
Document Modified: 2008-11-20 12:04:09
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