Attachment Sched S Tech Report

This document pretains to SAT-LOA-20100409-00072 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2010040900072_810336

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: SIRIUS FM-6 3/15/2012 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 12/28/2007 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 2/10/2011 3 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: 10/21/2011 3/1/2012 12.5 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) 2320.0 M 2332.5 M T Satellite Digital Audio Radio Service 7060.0 M 7072.5 M R Fixed Satellite Service 7051.5 M 7052.5 M R Fixed Satellite Service 7055.5 M 7056.5 M R Fixed Satellite Service 2321.35 M 2321.65 M T Satellite Digital Audio Radio Service 2321.85 M 2322.15 M T Satellite Digital Audio Radio Service 2330.35 M 2330.65 M T Satellite Digital Audio Radio Service 2330.85 M 2331.15 M T Satellite Digital Audio Radio 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: 115.2 W The orbital location provides good satellite spatial Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be diversity for the eventual GEO constellation and N/S Station-Keeping provided (Optional): provides high elevation angles to all of CONUS, which d. Toward West: Degrees E/W 0.05 Degrees Tolerance: is very important for the link between the satellite and g. Westernmost: W e. Toward East: 0.05 Degrees the mobile user terminals in CONUS. The high 0.05 Degrees h. Easternmost: W elevation angle minimizes the risk of signal blockage due to buildings and foliage. 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) SA1S S CONUS SA2X S Eastern & Central CONUS

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) XU1 R 31 30.1 0.18 1 30 N SA2X 649 2.9 -108 20 0.5 SD1 T 34.7 26.5 0.18 1 30 N SA1S 1 1000 71.6 OMN R 9 -4 0 1 30 N SA2X 630 -19 OMN T 9 -4 0 1 30 N SA1S 6.9 4.1 15.1 SAT T 13.4 12.7 0 1 30 N SA1S 7 4 19.4

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) XU1 R C -115.2 XU1.gxt SD1 T C -115.2 SD1.gxt -120.8 -120.8 -120.8 -120.8 -120.8 SAT T C -115.2 SATM.gxt -161.2 -161.2 -161.2 -161.2 -161.2

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) U001 4500 R 7062.29 R C BL01 130 U001 XU1 D001 SD1 U002 4500 R 7070.21 R C BL02 130 U002 XU1 D002 SD1 D001 4500 T 2322.29 L C C001 CMD1 OMNX1 D002 4500 T 2330.21 L C C002 CMD2 OMNX1 CMD1 1000 R 7052.0 L T T001 TLM1 OMNS1 CMD2 1000 R 7056.0 L T T002 TLM2 OMNS1 TLM1 300 T 2321.5 R T T003 TLM3 OMNS1 TLM2 300 T 2322.0 R T T004 TLM4 OMNS1 TLM3 300 T 2330.5 R T T005 TLM1 SATM TLM4 300 T 2331.0 R T T006 TLM2 SATM U003 12500 R 7066.25 R C T007 TLM3 SATM D003 12500 T 2326.25 L C T008 TLM4 SATM BL03 130 U003 XU1 D003 SD1

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 4M50G7E 4500 4 7517 0.6667 5 D2 4M50G7E 4500 8 3758 0.3333 5

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) A1 1M00F1D 1000 TC 1 36.2 48.4 A2 300KG1D 300 TM 1 50.1 63.8

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) BL01 BL02 D1 1 S-band PRM 63.4 71.6 -120.8 -18.3 C001 C002 A1 1 X-band CMD 50.5 15.5 24.5 66 75 27.7 T001 T004 A2 1 S-band TLM 2.1 15.1 -165.5 19.4 T005 T008 A2 1 S-band TLM 18.7 19.4 -161.2 19.4

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 Remote Control (TT C) Location(s): S14a: Street Address: 24 Vernon Crossing Road S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Vernon Sussex NJ 07462 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 973-764-4021 E040363 Remote Control (TT C) Location(s): S14a: Street Address: 24 Vernon Crossing Road S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Vernon Sussex NJ 07462 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 973-764-4021 E060276 Remote Control (TT C) Location(s): S14a: Street Address: 2875 Fork Creek Church S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Ellenwood Clayton GA 30294 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 404-381-2001 E040204

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 2975 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3105 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6080 32.4 0.9 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 733 18 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 89 11.1 0.76 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): 12978 12978 12978 12978 Bus (Watts): (b): (g): (l): (q): 3493 1684 3493 1684 Total (Watts): (c): (h): (m): (r): 16471 14662 16471 14662 Solar Array (Watts): (d): (i): (n): (s): 20895 18499 18364 16403 Depth of Battery (e) (j) (o) (t) Discharge (%): 55.5 % 0 % 58.6 % 0 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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 NOX 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? YES NO X 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: 2010-04-12 10:46:22
Document Modified: 2010-04-12 10:46:22
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