Attachment Sched S Tech Report

This document pretains to SAT-AMD-20130716-00094 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2013071600094_1006820

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-45W 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: 36 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: 1296 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) 10950 M 11200 M T Direct to Home in the Fixed Fixed Satellite Service 10950 M 11200 M T Fixed Satellite Service 13750 M 14500 M R Fixed Satellite Service 11450 M 11700 M T Direct to Home in the Fixed Fixed Satellite Service 11450 M 11700 M T Fixed Satellite Service 11950 M 12200 M T Direct to Home in the Fixed Fixed Satellite Service 11950 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: 45.2 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) B S Brasil

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) TXV T 33.4 27.4 0.1 0.1 30 N 90 B 2.2 91.2 53 RXH R 36.9 30.9 0.1 0.1 30 N 0B 1000 6.9 -100 20 1 RXV R 36.9 30.9 0.1 0.1 30 N 90 B 1000 6.9 -100 20 1 T1H T 34.9 28.8 0.1 0.1 30 N 0B 1.8 72.4 53.5 T1V T 34.9 28.9 0.1 0.1 30 N 90 B 1.8 72.4 53.5 T2H T 37 31 0.1 0.1 30 N 0B 5.3 44.7 53.5 T2V T 37 31 0.1 0.1 30 N 90 B 5.3 44.7 53.5

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) RXH R C -45.2 DTV-45W Rx H-pol AMD.gxt RXV R C -45.2 DTV-45W Rx V-pol AMD.gxt T1H T C -45.2 DTV-45W Tx1 H-pol AMD.gxt -168.5 -168.5 -168.5 -168.5 -168.5 T1V T C -45.2 DTV-45W Tx1 V-pol AMD.gxt -168.5 -168.5 -168.5 -168.5 -168.5 T2H T C -45.2 DTV-45W Tx2 H-pol AMD.gxt -168.5 -168.5 -168.5 -168.5 -168.5 T2V T C -45.2 DTV-45W Tx2 V-pol AMD.gxt -168.5 -168.5 -168.5 -168.5 -168.5

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 V C TP001 120 RX001 RXV TX001 T1H RX003 36000 R 14060 V C TP003 120 RX003 RXV TX003 T1H RX005 36000 R 14100 V C TP005 120 RX005 RXV TX005 T1H RX007 36000 R 14140 V C TP007 120 RX007 RXV TX007 T1H RX009 36000 R 14180 V C TP009 120 RX009 RXV TX009 T1H RX011 36000 R 14220 V C TP011 120 RX011 RXV TX011 T1H RX013 36000 R 14260 V C TP013 120 RX013 RXV TX013 T1H RX015 36000 R 14300 V C TP015 120 RX015 RXV TX015 T1H RX017 36000 R 14340 V C TP017 120 RX017 RXV TX017 T1H RX019 36000 R 14380 V C TP019 120 RX019 RXV TX019 T1H RX021 36000 R 14420 V C TP021 120 RX021 RXV TX021 T1H RX023 36000 R 14460 V C TP023 120 RX023 RXV TX023 T1H RX002 36000 R 14020 H C TP025 120 RX025 RXV TX025 T2H RX004 36000 R 14060 H C TP027 120 RX027 RXV TX027 T2H RX006 36000 R 14100 H C TP029 120 RX029 RXV TX029 T2H RX008 36000 R 14140 H C TP031 120 RX031 RXV TX031 T2H RX010 36000 R 14180 H C TP033 120 RX033 RXV TX033 T2H RX012 36000 R 14220 H C TP035 120 RX035 RXV TX035 T2H RX014 36000 R 14260 H C TP002 120 RX002 RXH TX002 T1V RX016 36000 R 14300 H C TP004 120 RX004 RXH TX004 T1V RX018 36000 R 14340 H C TP006 120 RX006 RXH TX006 T1V RX020 36000 R 14380 H C TP008 120 RX008 RXH TX008 T1V RX022 36000 R 14420 H C TP010 120 RX010 RXH TX010 T1V RX024 36000 R 14460 H C TP012 120 RX012 RXH TX012 T1V TX001 36000 T 11470 H C TP014 120 RX014 RXH TX014 T1V TX003 36000 T 11510 H C TP016 120 RX016 RXH TX016 T1V TX005 36000 T 11550 H C TP018 120 RX018 RXH TX018 T1V TX007 36000 T 11590 H C TP020 120 RX020 RXH TX020 T1V TX009 36000 T 11630 H C TP022 120 RX022 RXH TX022 T1V TX011 36000 T 11670 H C TP024 120 RX024 RXH TX024 T1V

TX013 36000 T 11980 H C TP026 120 RX026 RXH TX026 T2V TX015 36000 T 12020 H C TP028 120 RX028 RXH TX028 T2V TX017 36000 T 12060 H C TP030 120 RX030 RXH TX030 T2V TX019 36000 T 12100 H C TP032 120 RX032 RXH TX032 T2V TX021 36000 T 12140 H C TP034 120 RX034 RXH TX034 T2V TX023 36000 T 12180 H C TP036 120 RX036 RXH TX036 T2V TX002 36000 T 11470 V C CMD1 CMD1 RXV TX004 36000 T 11510 V C CMD2 CMD2 RXH TX006 36000 T 11550 V C TLM1 TLM1 T1H TX008 36000 T 11590 V C TLM2 TLM2 T1H TX010 36000 T 11630 V C TX012 36000 T 11670 V C TX014 36000 T 11980 V C TX016 36000 T 12020 V C TX018 36000 T 12060 V C TX020 36000 T 12100 V C TX022 36000 T 12140 V C TX024 36000 T 12180 V C CMD1 1300 R 14497 V T CMD2 1300 R 14495 H T TLM1 106 T 11697 H T TLM2 106 T 11695 H T TX025 36000 T 10970 H C TX027 36000 T 11010 H C TX029 36000 T 11050 H C TX031 36000 T 11090 H C TX033 36000 T 11130 H C TX035 36000 T 11170 H C TX026 36000 T 10970 V C TX028 36000 T 11010 V C TX030 36000 T 11050 V C TX032 36000 T 11090 V C TX034 36000 T 11130 V C TX036 36000 T 11170 V C RX025 36000 R 13774 V C RX027 36000 R 13814 V C RX029 36000 R 13854 V C RX031 36000 R 13894 V C RX033 36000 R 13934 V C

RX035 36000 R 13974 V C RX026 36000 R 13774 H C RX028 36000 R 13814 H C RX030 36000 R 13854 H C RX032 36000 R 13894 H C RX034 36000 R 13934 H C RX036 36000 R 13974 H C

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 43560 0.726 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) 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) CMD1 CMD2 CMD 1 60.7 11.2 11.2 TLM1 TLM2 TLM 1 -160.2 36.9 TP001 TP036 M01 1 60.7 10.1 12.9 47.5 53.5 -148.9 14

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 2300 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3860 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6160 42 0.95 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 3510 10.2 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 67 7.6 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): 8750 8750 8750 8750 Bus (Watts): (b): (g): (l): (q): 1450 900 1400 700 Total (Watts): (c): (h): (m): (r): 10200 9650 10150 9450 Solar Array (Watts): (d): (i): (n): (s): 14750 13475 13275 12127 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?: 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: 2013-07-18 12:03:28
Document Modified: 2013-07-18 12:03:28
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