Attachment Sched S Tech Report

This document pretains to SAT-AMD-20120420-00070 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2012042000070_949454

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 KU-79W N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 24 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: 864 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) 11700 M 12200 M T Direct to Home in the Fixed Fixed Satellite Service 11700 M 12200 M T Fixed Satellite Service 14000 M 14500 M R 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: 79 W 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 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) USA S CONUS and Puerto Rico MEX S Mexico USMEX S Southern US and Mexico

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) UST T 35.8 27.8 0.1 0 30 Y 0 USA 3.6 66 54 USTV T 35.8 27.8 0.1 0 30 Y 90 USA 3.6 66 54 MTH T 34.5 28.5 0.1 0 30 Y 0 MEX 2.3 89 54 MTV T 34.5 28.5 0.1 0 30 Y 90 MEX 2.3 89 54 RXH R 36.5 30.5 0.1 0 30 Y 0 USMEX 700 8 -100 20 1 RXV R 36.5 30.5 0.1 0 30 Y 90 USMEX 700 8 -100 20 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) UST T C -79 US+PR_TX_H.gxt USTV T C -79 US+PR_TX_V.gxt MTH T C -79 Mexico TX_H_R1.gxt MTV T C -79 Mexico TX_V_R1.gxt RXH R C -79 US+Mexico_RX_H.gxt RXV R C -79 US+Mexico_RX_V.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) RX001 36000 R 14020 H C U0001 120 RX001 RXH TX001 USTV RX003 36000 R 14060 H C U0003 120 RX003 RXH TX003 USTV RX005 36000 R 14100 H C U0005 120 RX005 RXH TX005 USTV RX007 36000 R 14140 H C U0007 120 RX007 RXH TX007 USTV RX009 36000 R 14180 H C U0009 120 RX009 RXH TX009 USTV RX011 36000 R 14220 H C U0011 120 RX011 RXH TX011 USTV RX013 36000 R 14260 H C U0013 120 RX013 RXH TX013 USTV RX015 36000 R 14300 H C U0015 120 RX015 RXH TX015 USTV RX017 36000 R 14340 H C U0017 120 RX017 RXH TX017 USTV RX019 36000 R 14380 H C U0019 120 RX019 RXH TX019 USTV RX021 36000 R 14420 H C U0021 120 RX021 RXH TX021 USTV RX023 36000 R 14460 H C U0023 120 RX023 RXH TX023 USTV RX002 36000 R 14040 V C U0002 120 RX002 RXV TX002 USTH RX004 36000 R 14080 V C U0004 120 RX004 RXV TX004 USTH RX006 36000 R 14120 V C U0006 120 RX006 RXV TX006 USTH RX008 36000 R 14160 V C U0008 120 RX008 RXV TX008 USTH RX010 36000 R 14200 V C U0010 120 RX010 RXV TX010 USTH RX012 36000 R 14240 V C U0012 120 RX012 RXV TX012 USTH RX014 36000 R 14280 V C U0014 120 RX014 RXV TX014 USTH RX016 36000 R 14320 V C U0016 120 RX016 RXV TX016 USTH RX018 36000 R 14360 V C U0018 120 RX018 RXV TX018 USTH RX020 36000 R 14400 V C U0020 120 RX020 RXV TX020 USTH RX022 36000 R 14440 V C U0022 120 RX022 RXV TX022 USTH RX024 36000 R 14480 V C U0024 120 RX024 RXV TX024 USTH TX001 36000 T 11720 V C M0001 120 RX001 RXH TX001 MTV TX003 36000 T 11760 V C M0003 120 RX003 RXH TX003 MTV TX005 36000 T 11800 V C M0005 120 RX005 RXH TX005 MTV TX007 36000 T 11840 V C M0007 120 RX007 RXH TX007 MTV TX009 36000 T 11880 V C M0009 120 RX009 RXH TX009 MTV TX011 36000 T 11920 V C M0011 120 RX011 RXH TX011 MTV

TX013 36000 T 11960 V C M0013 120 RX013 RXH TX013 MTV TX015 36000 T 12000 V C M0015 120 RX015 RXH TX015 MTV TX017 36000 T 12040 V C M0017 120 RX017 RXH TX017 MTV TX019 36000 T 12080 V C M0019 120 RX019 RXH TX019 MTV TX021 36000 T 12120 V C M0021 120 RX021 RXH TX021 MTV TX023 36000 T 12160 V C M0023 120 RX023 RXH TX023 MTV TX002 36000 T 11740 H C M0002 120 RX002 RXV TX002 MTH TX004 36000 T 11780 H C M0004 120 RX004 RXV TX004 MTH TX006 36000 T 11820 H C M0006 120 RX006 RXV TX006 MTH TX008 36000 T 11860 H C M0008 120 RX008 RXV TX008 MTH TX010 36000 T 11900 H C M0010 120 RX010 RXV TX010 MTH TX012 36000 T 11940 H C M0012 120 RX012 RXV TX012 MTH TX014 36000 T 11980 H C M0014 120 RX014 RXV TX014 MTH TX016 36000 T 12020 H C M0016 120 RX016 RXV TX016 MTH TX018 36000 T 12060 H C M0018 120 RX018 RXV TX018 MTH TX020 36000 T 12100 H C M0020 120 RX020 RXV TX020 MTH TX022 36000 T 12140 H C M0022 120 RX022 RXV TX022 MTH TX024 36000 T 12180 H C M0024 120 RX024 RXV TX024 MTH CMD1 1300 R 14005 V T CMD1 CMD1 RXV CMD2 1300 R 14495 H T CMD2 CMD2 RXH TLM1 106 T 11704 H T TLM1 TLM1 USTH TLM2 106 T 11705 H T TLM2 TLM2 USTH

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) M01 36M0G7W 36000 4 60000 0.58 3.8 16

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 1M30F9D 1300 1 15 27.2 TLM 106KG9D 106 1 14 26.2

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. 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) M0001 M0024 M01 1 59.8 15 17 48 54 -124 14 U0001 U0024 M01 1 59.8 15 17 46 54 -124 14 CMD1 CMD2 CMD 1 59.8 12.2 12.2 TLM1 TLM2 TLM 1 15.3 15.3 35.9

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 1225 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1250 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2475 22.4 0.95 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 500 5.1 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 26 7.4 0.808 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): 4650 4650 4650 4650 Bus (Watts): (b): (g): (l): (q): 1375 940 1375 940 Total (Watts): (c): (h): (m): (r): 6025 5590 6025 5590 Solar Array (Watts): (d): (i): (n): (s): 6935 6220 6725 6005 Depth of Battery (e) (j) (o) (t) Discharge (%): 70 % 0 % 70 % 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 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: 2012-04-24 15:51:12
Document Modified: 2012-04-24 15:51:12
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