Attachment Sched S Tech Report.

This document pretains to SAT-MOD-20140902-00098 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2014090200098_1060113

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 Fixed Satellite Service 11700 M 12200 M T Direct to Home in the Fixed Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 17300 M 17800 M T Broadcasting Satellite Service - Video 24750 M 25250 M R Feeder Link for Broadcasting Satellite Service in FSS 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: 78.8 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) USMEX S Southern US, Mexico, Central America MEX+ S Mexico, Central America, part of Caribbean MEX S Mexico GBL Visible earth

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) RKV R 43.1 37.1 0.1 0.4 27 N 90 USMEX 813 14 -98 19 1 RKH R 43.1 37.1 0.1 0.4 27 N 0 USMEX 813 14 -98 19 1 RBR R 40.6 30.6 0.1 0.1 27 N MEX 912 11 -90 19 1 RBL R 40.6 30.6 0.1 0.1 27 N MEX 912 11 -90 19 1 TBR T 37.9 31.9 0.1 0.1 27 N MEX 2.9 28.8 52.5 TBL T 37.9 31.9 0.1 0.1 27 N MEX 2.9 28.8 52.5 TKV T 34.9 28.9 0.1 0.4 27 N 90 MEX+ 2.8 64.6 53 TKH T 34.9 28.9 0.1 0.4 27 N 0 MEX+ 2.8 64.6 53 CMD R 23.8 17.8 0.1 0.1 27 Y GBL 1000 -5.2 -96 TLM T 25.8 19.8 0.1 0.1 27 Y GBL 10 0.1 15

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) RKV R C -78.8 DIRECTV KU-79W_Ku RX_ V Pol.gxt RKH R C -78.8 DIRECTV KU-79W_Ku RX_H Pol.gxt TKV T C -78.8 DIRECTV KU-79W_Ku TX_V.gxt TKH T C -78.8 DIRECTV KU-79W_Ku TX_H.gxt RBR R C -78.8 DIRECTV KU-79W_RB RX_RHCP.gxt RBL R C -78.8 DIRECTV KU-79W_RB RX_LHCP.gxt TBR T C -78.8 DIRECTV KU-79W_RB TX_RHCP.gxt -135 -135 -135 -135 -135 TBL T C -78.8 DIRECTV KU-79W_RB TX_LHCP.gxt -135 -135 -135 -135 -135

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) KUR01 36000 R 14020 V C KU001 120 KUR01 RKV KUT01 TKH KUR02 36000 R 14060 V C KU002 120 KUR02 RKV KUT02 TKH KUR03 36000 R 14100 V C KU003 120 KUR03 RKV KUT03 TKH KUR04 36000 R 14140 V C KU004 120 KUR04 RKV KUT04 TKH KUR05 36000 R 14180 V C KU005 120 KUR05 RKV KUT05 TKH KUR06 36000 R 14220 V C KU006 120 KUR06 RKV KUT06 TKH KUR07 36000 R 14260 V C KU007 120 KUR07 RKV KUT07 TKH KUR08 36000 R 14300 V C KU008 120 KUR08 RKV KUT08 TKH KUR09 36000 R 14340 V C KU009 120 KUR09 RKV KUT09 TKH KUR10 36000 R 14380 V C KU010 120 KUR10 RKV KUT10 TKH KUR11 36000 R 14420 V C KU011 120 KUR11 RKV KUT11 TKH KUR12 36000 R 14460 V C KU012 120 KUR12 RKV KUT12 TKH KUR13 36000 R 14040 H C KU013 120 KUR13 RKH KUT13 TKV KUR14 36000 R 14080 H C KU014 120 KUR14 RKH KUT14 TKV KUR15 36000 R 14120 H C KU015 120 KUR15 RKH KUT15 TKV KUR16 36000 R 14160 H C KU016 120 KUR16 RKH KUT16 TKV KUR17 36000 R 14200 H C KU017 120 KUR17 RKH KUT17 TKV KUR18 36000 R 14240 H C KU018 120 KUR18 RKH KUT18 TKV KUR19 36000 R 14280 H C KU019 120 KUR19 RKH KUT19 TKV KUR20 36000 R 14320 H C KU020 120 KUR20 RKH KUT20 TKV KUR21 36000 R 14360 H C KU021 120 KUR21 RKH KUT21 TKV KUR22 36000 R 14400 H C KU022 120 KUR22 RKH KUT22 TKV KUR23 36000 R 14440 H C KU023 120 KUR23 RKH KUT23 TKV KUR24 36000 R 14480 H C KU024 120 KUR24 RKH KUT24 TKV KUT01 36000 T 11720 H C RB001 120 RBR01 RBR RBT01 TBR KUT02 36000 T 11760 H C RB003 120 RBR03 RBR RBT03 TBR KUT03 36000 T 11800 H C RB005 120 RBR05 RBR RBT05 TBR KUT04 36000 T 11840 H C RB007 120 RBR07 RBR RBT07 TBR KUT05 36000 T 11880 H C RB009 120 RBR09 RBR RBT09 TBR KUT06 36000 T 11920 H C RB011 120 RBR11 RBR RBT11 TBR

KUT07 36000 T 11960 H C RB013 120 RBR13 RBR RBT13 TBR KUT08 36000 T 12000 H C RB015 120 RBR15 RBR RBT15 TBR KUT09 36000 T 12040 H C RB017 120 RBR17 RBR RBT17 TBR KUT10 36000 T 12080 H C RB019 120 RBR19 RBR RBT19 TBR KUT11 36000 T 12120 H C RB021 120 RBR21 RBR RBT21 TBR KUT12 36000 T 12160 H C RB023 120 RBR23 RBR RBT23 TBR KUT13 36000 T 11740 V C RB002 120 RBR02 RBL RBT02 TBL KUT14 36000 T 11780 V C RB004 120 RBR04 RBL RBT04 TBL KUT15 36000 T 11820 V C RB006 120 RBR06 RBL RBT06 TBL KUT16 36000 T 11860 V C RB008 120 RBR08 RBL RBT08 TBL KUT17 36000 T 11900 V C RB010 120 RBR10 RBL RBT10 TBL KUT18 36000 T 11940 V C RB012 120 RBR12 RBL RBT12 TBL KUT19 36000 T 11980 V C RB014 120 RBR14 RBL RBT14 TBL KUT20 36000 T 12020 V C RB016 120 RBR16 RBL RBT16 TBL KUT21 36000 T 12060 V C RB018 120 RBR18 RBL RBT18 TBL KUT22 36000 T 12100 V C RB020 120 RBR20 RBL RBT20 TBL KUT23 36000 T 12140 V C RB022 120 RBR22 RBL RBT22 TBL KUT24 36000 T 12180 V C RB024 120 RBR24 RBL RBT24 TBL RBT01 36000 T 17326 R C CMD1 CMD1 CMD RBT03 36000 T 17366 R C CMD2 CMD2 CMD RBT05 36000 T 17406 R C TLM1 TLM1 TLM RBT07 36000 T 17446 R C TLM2 TLM2 TLM RBT09 36000 T 17486 R C BCN BCN TLM RBT11 36000 T 17526 R C RBT13 36000 T 17566 R C RBT15 36000 T 17606 R C RBT17 36000 T 17646 R C RBT19 36000 T 17686 R C RBT21 36000 T 17726 R C RBT23 36000 T 17766 R C RBT02 36000 T 17326 L C RBT04 36000 T 17366 L C RBT06 36000 T 17406 L C RBT08 36000 T 17446 L C RBT10 36000 T 17486 L C RBT12 36000 T 17526 L C RBT14 36000 T 17566 L C RBT16 36000 T 17606 L C RBT18 36000 T 17646 L C

RBT20 36000 T 17686 L C RBT22 36000 T 17726 L C RBT24 36000 T 17766 L C RBR01 36000 R 24776 R C RBR03 36000 R 24816 R C RBR05 36000 R 24856 R C RBR07 36000 R 24896 R C RBR09 36000 R 24936 R C RBR11 36000 R 24976 R C RBR13 36000 R 25016 R C RBR15 36000 R 25056 R C RBR17 36000 R 25096 R C RBR19 36000 R 25136 R C RBR21 36000 R 25176 R C RBR23 36000 R 25216 R C RBR02 36000 R 24776 L C RBR04 36000 R 24816 L C RBR06 36000 R 24856 L C RBR08 36000 R 24896 L C RBR10 36000 R 24936 L C RBR12 36000 R 24976 L C RBR14 36000 R 25016 L C RBR16 36000 R 25056 L C RBR18 36000 R 25096 L C RBR20 36000 R 25136 L C RBR22 36000 R 25176 L C RBR24 36000 R 25216 L C CMD1 1300 R 14000.5 H T CMD2 1300 R 14496.5 V T TLM1 106 T 11700.25 V T TLM2 106 T 11701.25 V T BCN 0.1 T 12199 H 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) M1 36M0G7W 36000 4 46480 0.7747 6.4 18.6

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 1M30F9D 1300 1 15.5 27.7 TLM 106KG9D 106 1 10 22.2

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) KU001 KU024 M1 1 59.8 8 10 47 53 15.2 RB001 RB024 M1 1 64.7 11 16 46.5 52.5 -125 21.4 CMD1 CMD2 CMD 1 59.8 6.2 32.2 TLM1 TLM2 TLM 1 10 15 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): #Error

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 1260 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1787 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3047 22.4 0.95 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 625 5.1 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 26 7.4 0.8 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 (%): 80 % 0 % 80 % 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: 2014-09-04 09:22:41
Document Modified: 2014-09-04 09:22:41
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