Attachment Completed Schedule S

This document pretains to SES-AMD-20100809-01021 for Amended Filing on a Satellite Earth Station filing.

IBFS_SESAMD2010080901021_834192

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: AMAZONAS-2 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 2/16/2007 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: 6/1/2009 11/30/2009 1500 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) 14 G 14.5 G R Fixed Satellite Service 11.7 G 12.2 G 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: 61 W This position was granted by Brasilian administration. Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Under this application, we are only seeking authority to N/S Station-Keeping provided (Optional): provide service to the U.S. territories in the standard d. Toward West: Degrees E/W 0.05 Degrees Tolerance: Ku band (14-14.5 GHz and 11.7-12.2 GHz). g. Westernmost: e. Toward East: 0.05 Degrees 0.07 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 (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) 1 S AMA2_NA_SA.gxt 01

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) KUR R 33 25 0.05 0.05 30 N 01 427 6.7 -98.7 18 1 KUR R 33 25 0.05 0.05 30 N 90 1 427 6.7 -98.7 18 1 KUT T 34.3 26.3 0.05 0.05 30 N 01 2.4 17.7 52 KUT T 34.3 26.3 0.05 0.05 30 N 90 1 2.4 17.7 52

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) KUR R C -61 AMA2_NA_RX_H_C.gxt KUR R X -61 AMA2_NA_RX_H_X.gxt KUT T C -61 AMA2_NA_TX_H_C.gxt -132 -132 -132 -132 -132 KUT T X -61 AMA2_NA_TX_H_X.gxt KUR R C -61 AMA2_NA_RX_V_C.gxt KUR R X -61 AMA2_NA_RX_V_X.gxt KUT T C -61 AMA2_NA_TX_V_C.gxt -132 -132 -132 -132 -132 KUT T X -61 AMA2_NA_TX_V_X.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) KT1 36000 T 11972 V C 1 130 KR1 KURH KT1 KUTV KT2 36000 T 12012 V C 2 130 KR2 KURH KT2 KUTV KT3 36000 T 12052 V C 3 130 KR3 KURH KT3 KUTV KT4 36000 T 12092 V C 4 130 KR4 KURH KT4 KUTV KT5 36000 T 12132 V C 5 130 KR5 KURH KT5 KUTV KT6 36000 T 12172 V C 6 130 KR6 KURH KT6 KUTV KT7 36000 T 11972 H C 7 130 KR7 KURV KT7 KUTH KT8 36000 T 12012 H C 8 130 KR8 KURV KT8 KUTH KT9 36000 T 12052 H C 9 130 KR9 KURV KT9 KUTH KT10 36000 T 12092 H C 10 130 KR10 KURV KT10 KUTH KT11 36000 T 12132 H C 11 130 KR11 KURV KT11 KUTH KT12 36000 T 12172 H C 12 130 KR12 KURV KT12 KUTH KT13 36000 T 11730 V C 13 130 KR13 KURH KT13 KUTV KT14 36000 T 11770 V C 14 130 KR14 KURH KT14 KUTV KT15 36000 T 11810 V C 15 130 KR15 KURH KT15 KUTV KT16 36000 T 11850 V C 16 130 KR16 KURH KT16 KUTV KT17 36000 T 11890 V C 17 130 KR17 KURH KT17 KUTV KT18 36000 T 11930 V C 18 130 KR18 KURH KT18 KUTV KT19 36000 T 11730 H C 19 130 KR19 KURV KT19 KUTH KT20 36000 T 11770 H C 20 130 KR20 KURV KT20 KUTH KT21 36000 T 11810 H C 21 130 KR21 KURV KT21 KUTH KT22 36000 T 11850 H C 22 130 KR22 KURV KT22 KUTH KT23 36000 T 11890 H C 23 130 KR23 KURV KT23 KUTH KT24 36000 T 11930 H C 24 130 KR24 KURV KT24 KUTH KR13 36000 R 14030 H C 25 130 KR25 KURH KT25 KUTV KR14 36000 R 14070 H C 26 130 KR26 KURH KT26 KUTV KR15 36000 R 14110 H C 27 130 KR27 KURH KT27 KUTV KR16 36000 R 14150 H C 28 130 KR28 KURH KT28 KUTV KR17 36000 R 14190 H C 29 130 KR29 KURH KT29 KUTV KR18 36000 R 14230 H C 30 130 KR30 KURH KT30 KUTV

KR19 36000 R 14030 V C 31 130 KR31 KURV KT31 KUTH KR20 36000 R 14070 V C 32 130 KR32 KURV KT32 KUTH KR21 36000 R 14110 V C 33 130 KR33 KURV KT33 KUTH KR22 36000 R 14150 V C 34 130 KR34 KURV KT34 KUTH KR23 36000 R 14190 V C 35 130 KR35 KURV KT35 KUTH KR24 36000 R 14230 V C 36 130 KR36 KURV KT36 KUTH KT25 36000 T 10975 V C KT26 36000 T 11015 V C KT27 36000 T 11055 V C KT28 36000 T 11095 V C KT29 36000 T 11135 V C KT30 36000 T 11175 V C KT31 36000 T 10975 H C KT32 36000 T 11015 H C KT33 36000 T 11055 H C KT34 36000 T 11095 H C KT35 36000 T 11135 H C KT36 36000 T 11175 H C KR25 36000 R 14271 H C KR26 36000 R 14311 H C KR27 36000 R 14351 H C KR28 36000 R 14391 H C KR29 36000 R 14431 H C KR1 36000 R 13772 H C KR2 36000 R 13812 H C KR3 36000 R 13852 H C KR4 36000 R 13892 H C KR5 36000 R 13932 H C KR6 36000 R 13972 H C KR7 36000 R 13772 V C KR8 36000 R 13812 V C KR9 36000 R 13852 V C KR10 36000 R 13892 V C KR11 36000 R 13932 V C KR12 36000 R 13972 V C KR30 36000 R 14471 H C KR31 36000 R 14271 V C KR32 36000 R 14311 V C KR33 36000 R 14351 V C

KR34 36000 R 14391 V C KR35 36000 R 14431 V C KR36 36000 R 14471 V 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) 1 1M80G7W 1800 4 2048 0.75 9 17.7 2 33M0G7W 33000 4 38010 0.75 6.1 18.3 3 7M89G7W 9000 8 11300 0.67 8 20.2 4 14K0G7W 14 4 11 0.5 6.8 19

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) 1 36 1 18 LINK_BUDGET 53.2 1.2 9.2 30 32 -132.5 30 1 36 2 1 LINK_BUDGET 53.2 11.8 19.8 41.7 43.7 -133.5 26 1 36 3 4 LINK_BUDGET 49.4 8.1 16.1 36.6 38.6 -132.4 26.5 1 36 4 2337 LINK_BUDGET 43.4 -17.9 -9.9 3.15 5.15 -138.3 33

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: PRAIA DO FLAMENGO 200 S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: RIO DE JANEIRO BRAZIL 22210-030 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +552198582255 Remote Control (TT C) Location(s): S14a: Street Address: CARRETERA M 220, KM 1,800 S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: ARGANDA DEL REY SPAIN 28500 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): +34918700160

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 2505 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2931 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5436 28 0.91 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 861 8.6 0.86 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 71.41 6.7 0.78 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): 12020 12020 12020 12020 Bus (Watts): (b): (g): (l): (q): 2408 1016 2386 1011 Total (Watts): (c): (h): (m): (r): 14428 13036 14406 13031 Solar Array (Watts): (d): (i): (n): (s): 16006 14348 15380 13966 Depth of Battery (e) (j) (o) (t) Discharge (%): 65 % % 69 % % 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? X YES NO 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: 2010-08-09 10:54:14
Document Modified: 2010-08-09 10:54:14
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