Attachment Sched S Tech Report

This document pretains to SAT-A/O-20120817-00137 for Authority to Operate on a Satellite Space Stations filing.

IBFS_SATAO2012081700137_964308

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: DIRECTV 1R 1/15/2013 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 4.5 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 32 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: 768 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 f. Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode 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 17.8 G R Feeder Link for Broadcasting Satellite Service in FSS 12.2 G 12.7 G T Broadcasting Satellite Service - Video 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: 56.16 E 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 1.4 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 Angle (o) Other Plane (Seconds) Node (Deg.) (Degrees) 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) RUS S Russia

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) Input (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Losses Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) (dB) Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dBW) Temp (k) (db/K) (dBW/m2) RUL R 34.3 28.3 1 30 N RUS 562 6.8 -103.8 15 1 RDL T 36.3 28.3 1 30 N RUS 1.5 200 57.8

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) RUL R C 56.16 RUL.gxt RDL T C 56.16 RDL.gxt

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 (T ID Gain (dB) No. ID No. or C) T0001 24000 T 12224 R C 00001 163 R0001 UL T0001 DL T0003 24000 T 12253.16 R C 00003 163 R0003 UL T0003 DL T0005 24000 T 12282.32 R C 00005 163 R0005 UL T0005 DL T0007 24000 T 12311.48 R C 00007 163 R0007 UL T0007 DL T0009 24000 T 12340.64 R C 00009 163 R0009 UL T0009 DL T0011 24000 T 12369.8 R C 00011 163 R0011 UL T0011 DL T0013 24000 T 12398.96 R C 00013 163 R0013 UL T0013 DL T0015 24000 T 12428.12 R C 00015 163 R0015 UL T0015 DL T0017 24000 T 12457.28 R C 00017 163 R0017 UL T0017 DL T0019 24000 T 12486.44 R C 00019 163 R0019 UL T0019 DL T0021 24000 T 12515.6 R C 00021 163 R0021 UL T0021 DL T0023 24000 T 12544.76 R C 00023 163 R0023 UL T0023 DL T0025 24000 T 12573.92 R C 00025 163 R0025 UL T0025 DL T0027 24000 T 12603.08 R C 00027 163 R0027 UL T0027 DL T0029 24000 T 12632.24 R C 00029 163 R0029 UL T0029 DL T0031 24000 T 12661.4 R C 00031 163 R0031 UL T0031 DL T0002 24000 T 12238.58 L C 00002 163 R0002 UL T0002 DL T0004 24000 T 12267.74 L C 00004 163 R0004 UL T0004 DL T0006 24000 T 12296.9 L C 00006 163 R0006 UL T0006 DL T0008 24000 T 12326.06 L C 00008 163 R0008 UL T0008 DL T0010 24000 T 12355.22 L C 00010 163 R0010 UL T0010 DL T0012 24000 T 12384.38 L C 00012 163 R0012 UL T0012 DL T0014 24000 T 12413.54 L C 00014 163 R0014 UL T0014 DL T0016 24000 T 12442.7 L C 00016 163 R0016 UL T0016 DL T0018 24000 T 12471.86 L C 00018 163 R0018 UL T0018 DL T0020 24000 T 12501.02 L C 00020 163 R0020 UL T0020 DL T0022 24000 T 12530.18 L C 00022 163 R0022 UL T0022 DL T0024 24000 T 12559.34 L C 00024 163 R0024 UL T0024 DL T0026 24000 T 12588.5 L C 00026 163 R0026 UL T0026 DL T0028 24000 T 12617.66 L C 00028 163 R0028 UL T0028 DL

T0030 24000 T 12646.82 L C 00030 163 R0030 UL T0030 DL T0032 24000 T 12675.98 L C 00032 163 R0032 UL T0032 DL R0001 24000 R 17324 R C TLM1 TLM1 DL R0003 24000 R 17353.16 R C TLM2 TLM2 DL R0005 24000 R 17382.32 R C R0007 24000 R 17411.48 R C R0009 24000 R 17440.64 R C R0011 24000 R 17469.8 R C R0013 24000 R 17498.96 R C R0015 24000 R 17528.12 R C R0017 24000 R 17557.28 R C R0019 24000 R 17586.44 R C R0021 24000 R 17615.6 R C R0023 24000 R 17644.76 R C R0025 24000 R 17673.92 R C R0027 24000 R 17703.08 R C R0029 24000 R 17732.24 R C R0031 24000 R 17761.4 R C R0002 24000 R 17338.58 L C R0004 24000 R 17367.74 L C R0006 24000 R 17396.9 L C R0008 24000 R 17426.06 L C R0010 24000 R 17455.22 L C R0012 24000 R 17484.38 L C R0014 24000 R 17513.54 L C R0016 24000 R 17542.7 L C R0018 24000 R 17571.86 L C R0020 24000 R 17601.02 L C R0022 24000 R 17630.18 L C R0024 24000 R 17659.34 L C R0026 24000 R 17688.5 L C R0028 24000 R 17717.66 L C R0030 24000 R 17746.82 L C R0032 24000 R 17775.98 L C CMD1 800 R 17305.0 R T CMD2 800 R 17799.0 R T TLM1 800 T 12699.25 R T TLM2 800 T 12698.25 L 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) DTH1 24M0G7W 24000 4 18440 0.461 3.4 15.6

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) CMD 800KF2D 800 1 7.6 19.8 TLM 800KF2D 800 1 7.6 19.8

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. Power (o)Assoc. Transponder (kHz) No.) Bandwidth (Table S11) (Table S12) Stn. Max. Power (dBW) Flux Density Stn Rec. (a) Start (b) End (kHz) Antenna (dBW/m2/Hz) G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dB/K) 00001 00032 DTH1 1 49.8 57.8 11 TLM1 TLM2 TLM 1 -4 16 39 00001 00032 DTH1 49.8 57.8 14.5

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: 1600 Forbes Way S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Long Beach Los Angeles CA 90810 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 310 525 5590 Remote Control (TT C) Location(s): S14a: Street Address: 3400 International Drive S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Washington DC DC 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202 944 7701

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 1741 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1786 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3527 26.2 0.93 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 526 2.2 0.89 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 43.9 8.1 0.83 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): 5928 5928 5928 5928 Bus (Watts): (b): (g): (l): (q): 1621 704 1552 908 Total (Watts): (c): (h): (m): (r): 7549 6632 7480 6836 Solar Array (Watts): (d): (i): (n): (s): 8653 7702 7702 7031 Depth of Battery (e) (j) (o) (t) Discharge (%): 70.4 % 70.4 % 77.2 % 77.2 % 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 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: 2012-08-22 16:32:14
Document Modified: 2012-08-22 16:32:14
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