Attachment Sched S Tech Report.

This document pretains to SAT-LOA-20140114-00005 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2014011400005_1033027

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: INTELSAT 34 10/1/2015 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 6/20/2013 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 6/20/2015 40 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: 7/27/2015 1/27/2016 1738 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) 5925 M 6425 M R Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 11450 M 11700 M T Fixed Satellite Service 11700 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: 55.5 W REPLACE EXISTING INTELSAT 805 AND GALAXY Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be 11 SPACECRAFT 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) 1 S NORTH AND SOUTH AMERICA AND EUROPE 2 S BRAZIL 3 S UNITED STATES, MEXICO, CENTRAL AMERICA, CARIBBEAN, EUROPE, ATLANTIC OCEAN 4 S GLOBAL

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) HHU R 28.2 22.3 0.1 0.2 30 N 01 531 1 -104 25 1 HVUL R 28.2 22.3 0.1 0.2 30 N 90 1 531 0.9 -104.9 25 1 BHUL R 36.5 31.3 0.1 0.2 30 N 02 708 8 -103 21 1 BVUL R 36.5 31.3 0.1 0.2 30 N 90 2 708 8 -103 21 1 NHU R 28.3 23 0.1 0.2 30 N 03 589 0.6 -95.6 21 1 HHD T 25.6 21.6 0.1 0.2 30 N 01 2.5 65 41.2 HVDL T 25.5 21.5 0.1 0.2 30 N 90 1 2.5 65 41.1 BHDL T 35.5 29.8 0.1 0.2 30 N 02 2.9 150 54.4 BVDL T 35.5 29.8 0.1 0.2 30 N 90 2 2.9 150 54.4 NVDL T 28.2 22.6 0.1 0.2 30 N 90 3 3.2 150 46.8 CMD R 28.2 22.3 0.1 0.2 N 01 5146 -8.9 -124.4 CMD R 2 -2.1 0.1 0.2 N 4 4925 -34.9 -96.4 TLMV T 25.5 21.5 0.1 0.2 N 90 1 9.7 0.5 9.6 TLMB T 6 3.4 0.1 0.2 N 4 10 45 12.5 UPC T 24.9 20.8 0.1 0.2 N 04 5.6 0.4 15.3 UPK T 21.5 17.4 0.1 0.2 N 90 4 2 0.5 16.5 UPK T 22 17.9 0.1 0.2 N 04 2 0.5 17

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) HHU R C -55.5 hhul.gxt HVUL R C -55.5 hvul.gxt BHUL R C -55.5 bhul.gxt BVUL R C -55.5 bvul.gxt NHU R C -55.5 nhul.gxt HHD T C -55.5 hhdl.gxt -152.1 -152 -151.8 -151.7 -151.6 HVDL T C -55.5 hvdl.gxt -152.2 -152.1 -151.9 -151.8 -151.7 BHDL T C -55.5 bhdl.gxt BVDL T C -55.5 bvdl.gxt NVDL T C -55.5 nvdl.gxt -150 -147.5 -146.2 -146.1 -146 CMD R C -55.5 cmdh.gxt CMD R C -55.5 cmdb.gxt TLMV T C -55.5 TLMV.gxt -166.2 -166.1 -166 -165.9 -165.8 TLMB T C -55.5 tlmb.gxt -170.9 -170.8 -170.7 -170.6 -170.5 UPC T C -55.5 upch.gxt -155.9 -155.8 -155.7 -155.6 -155.5 UPK T C -55.5 upkh.gxt -154.2 -154.1 -154 -153.9 -153.8 UPK T C -55.5 upkv.gxt -154.7 -154.6 -154.5 -154.4 -154.3

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) 1CU 72000 R 5970 H C C0001 129.6 1CU HHUL 1CD HVDL 3CU 36000 R 6030 H C C0003 129.6 3CU HHUL 3CD HVDL 5CU 36000 R 6070 H C C0005 129.6 5CU HHUL 5CD HVDL 7CU 36000 R 6110 H C C0007 129.6 7CU HHUL 7CD HVDL 9CU 36000 R 6150 H C C0009 129.6 9CU HHUL 9CD HVDL 11CU 36000 R 6200 H C C0011 129.6 11CU HHUL 11CD HVDL 13CU 36000 R 6240 H C C0013 129.6 13CU HHUL 13CD HVDL 15CU 36000 R 6280 H C C0015 129.6 15CU HHUL 15CD HVDL 17CU 36000 R 6320 H C C0017 129.6 17CU HHUL 17CD HVDL 19CU 36000 R 6360 H C C0019 129.6 19CU HHUL 19CD HVDL 2CU 72000 R 5970 V C C0002 129.6 2CU HVUL 2CD HHDL 4CU 36000 R 6030 V C C0004 129.6 4CU HVUL 4CD HHDL 6CU 36000 R 6070 V C C0006 129.6 6CU HVUL 6CD HHDL 8CU 36000 R 6110 V C C0008 129.6 8CU HVUL 8CD HHDL 10CU 36000 R 6150 V C C0010 129.6 10CU HVUL 10CD HHDL 12CU 36000 R 6200 V C C0012 129.6 12CU HVUL 12CD HHDL 14CU 36000 R 6240 V C C0014 129.6 14CU HVUL 14CD HHDL 16CU 36000 R 6280 V C C0016 129.6 16CU HVUL 16CD HHDL 18CU 36000 R 6320 V C C0018 129.6 18CU HVUL 18CD HHDL 20CU 36000 R 6360 V C C0020 129.6 20CU HVUL 20CD HHDL 1CD 72000 T 3745 V C BB001 129.8 1KU BHUL 1KD BVDL 3CD 36000 T 3805 V C BB003 129.8 3KU BHUL 3KD BVDL 5CD 36000 T 3845 V C BB005 129.8 5KU BHUL 5KD BVDL 7CD 36000 T 3885 V C BB002 129.8 2KU BVUL 2KD BHDL 9CD 36000 T 3925 V C BB004 129.8 4KU BVUL 4KD BHDL 11CD 36000 T 3975 V C BB006 129.8 6KU BVUL 6KD BHDL 13CD 36000 T 4015 V C BB008 129.8 8KU BVUL 8KD BHDL 15CD 36000 T 4055 V C BB010 139.8 10KU BVUL 10KD BHDL 17CD 36000 T 4095 V C BB012 139.8 12KU BVUL 12KD BHDL 19CD 36000 T 4135 V C BB014 139.8 14KU BVUL 14KD BHDL

2CD 72000 T 3745 H C BB016 139.8 16KU BVUL 16KD BHDL 4CD 36000 T 3805 H C BB018 139.8 18KU BVUL 18KD BHDL 6CD 36000 T 3845 H C BB020 139.8 20KU BVUL 20KD BHDL 8CD 36000 T 3885 H C C0021 129.6 21CU HHUL 21CD HHDL 10CD 36000 T 3925 H C C0022 129.6 22CU HHUL 22CD HHDL 12CD 36000 T 3975 H C BB007 129.8 7KU BHUL 7KD BVDL 14CD 36000 T 4015 H C BB009 129.8 9KU BHUL 9KD BVDL 16CD 36000 T 4055 H C BB011 129.8 11KU BHUL 11KD BVDL 18CD 36000 T 4095 H C BB013 129.8 13KU BHUL 13KD BVDL 20CD 36000 T 4135 H C BB015 129.8 15KU BHUL 15KD BVDL 1KU 72000 R 14045 H C NN017 136.3 17KU NHUL 17KD NVDL 3KU 36000 R 14105 H C NN019 136.3 19KU NHUL 19KD NVDL 5KU 36000 R 14145 H C NN021 136.3 21KU NHUL 21KD NVDL 7KU 36000 R 14195 H C NN023 136.3 23KU NHUL 23KD NVDL 9KU 36000 R 14225 H C NN025 136.3 25KU NHUL 25KD NVDL 11KU 72000 R 14290 H C 13KU 72000 R 14370 H C 15KU 72000 R 14450 H C 17KU 72000 R 14045 H C 19KU 36000 R 14105 H C 2KU 72000 R 14045 V C 4KU 72000 R 14125 V C 6KU 36000 R 14190 V C 8KU 36000 R 14230 V C 10KU 36000 R 14270 V C 12KU 36000 R 14310 V C 14KU 36000 R 14350 V C 16KU 36000 R 14390 V C 18KU 36000 R 14430 V C 20KU 36000 R 14470 V C 1KD 72000 T 11990 V C 3KD 36000 T 12050 V C 5KD 36000 T 12090 V C 7KD 36000 T 12130 V C 9KD 36000 T 12170 V C 11KD 72000 T 11745 V C 13KD 72000 T 11825 V C 15KD 72000 T 11905 V C 17KD 72000 T 11495 V C

19KD 36000 T 11555 V C 2KD 72000 T 11745 H C 4KD 72000 T 11825 H C 6KD 36000 T 11890 H C 8KD 36000 T 11930 H C 10KD 36000 T 11970 H C 12KD 36000 T 12010 H C 14KD 36000 T 12050 H C 16KD 36000 T 12090 H C 18KD 36000 T 12130 H C 20KD 36000 T 12170 H C CMD1 1000 R 6173.7 H T CMD2 1000 R 6176.3 H T TM1 500 T 3949 V T TM2 500 T 3949.5 V T TM3 500 T 3950.5 V T TM4 500 T 3951 V T TM5 500 T 3949 R T TM6 500 T 3949.5 R T TM7 500 T 3950.5 R T TM8 500 T 3951 R T UPC1 25 T 3700.25 H T UPK1 25 T 11699.25 V T UPK2 25 T 11699.5 H T 21KD 36000 T 11595 V C 23KD 36000 T 11635 V C 25KD 36000 T 11675 V C 21CU 41000 R 6402.5 H C 22CU 41000 R 6402.5 V C CMD3 1000 R 6173.7 L T CMD4 1000 R 6176.3 L T 21CD 41000 T 4177.5 V C 22CD 41000 T 4177.5 H C 21KU 36000 R 11595 H C 23KU 36000 R 11635 H C 25KU 36000 R 11675 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) D1 72M0G7W 72000 4 49150 0.5 4.5 20.2 D2 8M7G7W 8789.5 4 6000 0.5 4.5 30 D3 323KG7W 323.5 4 256 0.5 3 23.2 D4 5M33G7W 5333 2 512 0.5 -5.2 24.5 D5 1M33G7W 1333.5 2 128 0.5 -5.2 22.3

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 36M0F3F 36000 TV/FM 1 NTSC 12.8 2.6 15.4 25.5

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) C0001 C0022 A1 1 C-Band Link Bu 4000 56.7 19.3 25.2 31.2 37.1 -156 31.7 C0001 C0022 D1 1 C-Band Link Bu 51.2 18.5 24.4 31.1 37 -167.4 22.7 C0001 C0022 D2 8 C-Band Link Bu 48.6 19 24.9 18.7 24.6 -170.6 22.7 C0001 C0022 D3 223 C-Band Link Bu 45.1 7.2 13.1 3.4 9.3 -172.1 22.7 BB001 BB015 A1 1 Brazil Link Bud 4000 53.1 16.9 22.1 42.5 47.7 -152.7 29 BB001 BB015 D1 1 Brazil Link Bud 53.1 18.3 23.5 40.3 45.5 -166.1 23.3 BB001 BB015 D2 8 Brazil Link Bud 46.6 10.5 15.7 30.9 36.1 -166.4 23.3 BB001 BB015 D3 223 Brazil Link Bud 46.6 -4.5 0.7 15.8 21 -167.7 23.3 BB001 BB015 D4 14 Brazil Link Bud 46.6 8.8 14 29.2 34.4 -166.4 16.5 BB001 BB015 D5 54 Brazil Link Bud 46.6 2.9 8.1 23.2 28.4 -166.4 16.5 NN017 NN025 A1 1 NAOR Link Bud 4000 57.4 16.9 22.2 35.2 40.8 -159.5 39 NN017 NN025 D1 1 NAOR Link Bud 48.7 18.3 23.6 35.5 41.1 -170.4 29.5 NN017 NN025 D2 8 NAOR Link Bud 53 17.8 24.2 23.9 29.5 -172.9 29 NN017 NN025 D3 223 NAOR Link Bud 53 -2.6 2.7 8.7 14.3 -174.3 29 NN017 NN025 D4 14 NAOR Link Bud 49.1 9 14.3 16.3 21.9 -178.9 25 NN017 NN025 D5 54 NAOR Link Bud 49.1 3 8.3 10.4 16 -178.7 25

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: 3400 INTERNATIONAL DRIVE, NW S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: WASHINGTON 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 1818 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1482 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3300 24.7 0.926 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 190 9.5 0.863 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 22.4 5.8 0.753 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): 6623 6623 6623 6623 Bus (Watts): (b): (g): (l): (q): 1860 1199 1763 1118 Total (Watts): (c): (h): (m): (r): 8483 7822 8483 7822 Solar Array (Watts): (d): (i): (n): (s): 10913 9709 10015 9023 Depth of Battery (e) (j) (o) (t) Discharge (%): 71.2 % % 71.2 % % 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: 2014-01-15 10:35:29
Document Modified: 2014-01-15 10:35:29
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