Attachment Sched S Tech Report

This document pretains to SES-LIC-20110408-00426 for License on a Satellite Earth Station filing.

IBFS_SESLIC2011040800426_884400

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: 10 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 540 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) 6725 M 7025 M R Fixed Satellite Service 4500 M 4800 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: 61 W This position was granted by French administration. 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 0.07 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 AMA-2.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) 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) CRH R 25.5 15.5 0.05 0.05 30 N 01 446 -1 -97 20 1 CRV R 25.5 15.5 0.05 0.05 30 N 90 1 446 -1 -97 20 1 CTH T 25.3 15.3 0.05 0.05 30 N 01 1.5 15.7 41 CTV T 25.3 15.3 0.05 0.05 30 N 90 1 1.5 15.7 41

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) CRH R C -61 Copol G_T_H.gxt CRH R X -61 Cross G_T_H.gxt CTH T C -61 Copol PIRE_H.gxt -157.68 -157.68 -157.68 -157.68 -157.68 CTH T X -61 Cross PIRE_H.gxt CRV R C -61 Copol G_T_V.gxt CRV R X -61 Cross G_T_V.gxt CTV T C -61 Copol PIRE_V.gxt -157.68 -157.68 -157.68 -157.68 -157.68 CTV T X -61 Cross PIRE_V.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 (T ID Gain (dB) No. ID No. or C) CT1 54000 T 4532.5 V C 1 124 CR1 CRH CT1 CTV CT2 54000 T 4592.5 V C 2 124 CR2 CRH CT2 CTV CT3 54000 T 4652.5 V C 3 124 CR3 CRH CT3 CTV CT4 54000 T 4712.5 V C 4 124 CR4 CRH CT4 CTV CT5 54000 T 4772.5 V C 5 124 CR5 CRH CT5 CTV CT6 54000 T 4532.5 H C 6 124 CR6 CRV CT6 CTH CT7 54000 T 4592.5 H C 7 124 CR7 CRV CT7 CTH CT8 54000 T 4652.5 H C 8 124 CR8 CRV CT8 CTH CT9 54000 T 4712.5 H C 9 124 CR9 CRV CT9 CTH CT10 54000 T 4772.5 H C 10 124 CR10 CRV CT10 CTH CR1 54000 R 6755 H C CR2 54000 R 6815 H C CR3 54000 R 6875 H C CR4 54000 R 6935 H C CR5 54000 R 6995 H C CR6 54000 R 6755 V C CR7 54000 R 6815 V C CR8 54000 R 6875 V C CR9 54000 R 6935 V C CR10 54000 R 6995 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 60K0G7W 70 8 64 0.6667 8 20.2 2 1M50G7W 1700 8 2048 0.6667 8 20.2 3 6M80G7W 7500 4 8448 0.75 9 21.2 4 33M0G7W 36000 4 45000 0.875 7.4 19.6

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)

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 S11) (Table S12) Stn. Max. Power (dBW) Power Flux Stn (a) Start (b) End (kHz) Antenna Density Rec. G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dBW/m2/Hz) (dB/K) 1 10 1 635 LINK_BUDGET 48.4 -8 2 4.3 10.3 -164.2 24.5 1 10 1 481 LINK_BUDGET 48.4 -7 3 6 12 -162.5 23 1 10 2 28 LINK_BUDGET 48.4 6.2 16.2 18 24 -167.3 26.5 1 10 2 14 LINK_BUDGET 48.4 10 20 21 27 -161.3 23 1 10 3 5 LINK_BUDGET 48.4 12.4 23.4 25.7 31.7 -163 26.5 1 10 4 1 LINK_BUDGET 48.4 15.7 25.7 28.8 34.8 -166.7 31

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: 2011-04-20 09:06:50
Document Modified: 2011-04-20 09:06:50
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