Attachment Schedule S Tech Data

This document pretains to SES-MFS-20050624-00813 for Modification w/ Foreign Satellite (earth station) on a Satellite Earth Station filing.

IBFS_SESMFS2005062400813_440524

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: AMC-16 7/1/2005 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 24 0 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 Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode f. 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) 14000 M 14500 M R Feeder Link for Broadcasting Satellite Service in FSS 11700 M 12200 M T Direct to Home in the Fixed 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: 118.75 W The 118.7° W.L orbital location is consistent with the Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Trilateral Agreement reached between Canada, N/S Station-Keeping provided (Optional): Mexico and the United States of America in 1988. It is d. Toward West: Degrees E/W 0.05 Degrees Tolerance: proposed to operate the AMC-16 satellite 0.05° to t he g. Westernmost: e. Toward East: 0.05 Degrees west to facilitate operation with the collocated Anik E2 0.1 Degrees h. Easternmost: satellite. 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 (o) Other Plane (Seconds) Node (Deg.) (Degrees) Angle 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) SAUP S CONUS, Hawaii SADN S CONUS

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) (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Input Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) Losses Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) (db/K) (dBW/m2) NAL R 33.3 26.3 0.15 30 Y 0 SAUP 594 5.6 -98.6 18 1 NALV R 33.3 26.3 0.15 30 Y 90 SAUP 594 5.6 -98.6 18 1 NAC T 37.1 26.7 0.15 30 Y SADN 2.3 83.2 56.3 NAC T 37.1 26.7 0.15 30 Y SADN 2.3 83.2 56.3

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) NAL R C -118.75 NALH.gxt NALV R C -118.75 NALV.gxt NAC T C -118.75 NACL.gxt NAC T C -118.75 NACR.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 ID Gain (dB) No. ID No. (T or C) UH001 36000 R 14020 H C T0001 130 UH001 NALH DR001 NACR UH003 36000 R 14060 H C T0003 130 UH003 NALH DR003 NACR UH005 36000 R 14100 H C T0005 130 UH005 NALH DR005 NACR UH007 36000 R 14140 H C T0007 130 UH007 NALH DR007 NACR UH009 36000 R 14180 H C T0009 130 UH009 NALH DR009 NACR UH011 36000 R 14220 H C T0011 130 UH011 NALH DR011 NACR UH013 36000 R 14260 H C T0013 130 UH013 NALH DR013 NACR UH015 36000 R 14300 H C T0015 130 UH015 NALH DR015 NACR UH017 36000 R 14340 H C T0017 130 UH017 NALH DR017 NACR UH019 36000 R 14380 H C T0019 130 UH019 NALH DR019 NACR UH021 36000 R 14420 H C T0021 130 UH021 NALH DR021 NACR UH023 36000 R 14460 H C T0023 130 UH023 NALH DR023 NACR UV002 36000 R 14040 V C T0002 130 UV002 NALV DL002 NACL UV004 36000 R 14080 V C T0004 130 UV004 NALV DL004 NACL UV006 36000 R 14120 V C T0006 130 UV006 NALV DL006 NACL UV008 36000 R 14160 V C T0008 130 UV008 NALV DL008 NACL UV010 36000 R 14200 V C T0010 130 UV010 NALV DL010 NACL UV012 36000 R 14240 V C T0012 130 UV012 NALV DL012 NACL UV014 36000 R 14280 V C T0014 130 UV014 NALV DL014 NACL UV016 36000 R 14320 V C T0016 130 UV016 NALV DL016 NACL UV018 36000 R 14360 V C T0018 130 UV018 NALV DL018 NACL UV020 36000 R 14400 V C T0020 130 UV020 NALV DL020 NACL UV022 36000 R 14440 V C T0022 130 UV022 NALV DL022 NACL UV024 36000 R 14480 V C T0024 130 UV024 NALV DL024 NACL DR001 36000 T 11720 R C DR003 36000 T 11760 R C DR005 36000 T 11800 R C DR007 36000 T 11840 R C DR009 36000 T 11880 R C DR011 36000 T 11920 R C

DR013 36000 T 11960 R C DR015 36000 T 12000 R C DR017 36000 T 12040 R C DR019 36000 T 12080 R C DR021 36000 T 12120 R C DR023 36000 T 12160 R C DL002 36000 T 11740 L C DL004 36000 T 11780 L C DL006 36000 T 11820 L C DL008 36000 T 11860 L C DL010 36000 T 11900 L C DL012 36000 T 11940 L C DL014 36000 T 11980 L C DL016 36000 T 12020 L C DL018 36000 T 12060 L C DL020 36000 T 12100 L C DL022 36000 T 12140 L C DL024 36000 T 12180 L 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 31M2G7W 31200 4 35940 0.691 6.1 18.3

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)

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. (o)Assoc. Transponder (kHz) No.) Bandwidth (Table (Table S12) Stn. Max. Power (dBW) Power Flux Stn (a) Start (b) End (kHz) S11) Antenna Density Rec. G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dBW/m2/Hz) (dB/K) T0001 T0024 D1 1 LB1.doc 63.2 11.4 19.4 42.3 52.3 -145 15.1

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 1952 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2133 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4065 27 0.7897 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 680 7 0.882 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 71.33 4.5 0.6965 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): 7503 7503 7503 7503 Bus (Watts): (b): (g): (l): (q): 551.7 541.9 548.6 533.7 Total (Watts): (c): (h): (m): (r): 8054.7 8044.9 8051.6 8036.7 Solar Array (Watts): (d): (i): (n): (s): 12425 11070 10520 9440 Depth of Battery (e) (j) (o) (t) Discharge (%): 72.6 % % 75.4 % % 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: 2005-07-08 18:23:06
Document Modified: 2005-07-08 18:23:06
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