Attachment Sched S Tech Report

This document pretains to SAT-PPL-20120418-00069 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2012041800069_949441

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-3 3/31/2013 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 5/31/2010 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 8 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: 12/1/2012 5/31/2013 3600 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) 18300 M 18800 M T Fixed Satellite Service 19700 M 20200 M T Fixed Satellite Service 28100 M 28600 M R Fixed Satellite Service 29500 M 30000 M R 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 The satellite network AMAZONAS-3 will be a Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be replacement of the AMAZONAS-1 (located in the N/S Station-Keeping provided (Optional): orbital location 61º West) in the C and Ku bands and d. Toward West: Degrees E/W 0.05 Degrees Tolerance: will add new Ka band capacity. Under this application, g. Westernmost: e. Toward East: 0.05 Degrees we are only seeking authority to provide service with 0.07 Degrees h. Easternmost: AMAZONAS-3 to the U.S. territories in the standard bands. 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 AMA-3_1.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) FW3 R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW5 R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 RT3D T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT5D T 48 43 0.1 0.1 26 N 1 2.5 17 65 FW1 R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW6 R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 RT1D T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT6D T 48 43 0.1 0.1 26 N 1 2.5 17 65 FW3 T 48 43 0.1 0.1 26 N 1 2.5 17 65 FW5 T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT3U R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 RT5U R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW7 T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT7U R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW6 T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT6U R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW1 T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT1U R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW9 T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT9U R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW8 T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT8U R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW2 T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT2U R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW2 R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 FW9 R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 RT2D T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT9D T 48 43 0.1 0.1 26 N 1 2.5 17 65 FW7 R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5

FW8 R 52 47 0.1 0.1 26 N 1 2570 18 -95 20 0.5 RT7D T 48 43 0.1 0.1 26 N 1 2.5 17 65 RT8D T 48 43 0.1 0.1 26 N 1 2.5 17 65

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) FW3 R C -61 FW3U_C.gxt FW3 R X -61 FW3U_X.gxt RT3D T C -61 RT3D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 RT3D T X -61 RT3D_X.gxt FW5 R C -61 FW5U_C.gxt FW5 R X -61 FW5U_X.gxt RT5D T C -61 RT5D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 RT5D T X -61 RT5D_X.gxt RT1U R C -61 RT1U_C.gxt RT1U R X -61 RT1U_X.gxt FW1 T C -61 FW1D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 FW1 T X -61 FW1D_X.gxt RT2U R C -61 RT2U_C.gxt RT2U R X -61 RT2U_X.gxt FW2 T C -61 FW2D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 FW2 T X -61 FW2D_X.gxt RT3U R C -61 RT3U_C.gxt RT3U R X -61 RT3U_X.gxt FW3 T C -61 FW3D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 FW3 T X -61 FW3D_X.gxt RT5U R C -61 RT5U_C.gxt RT5U R X -61 RT5U_X.gxt FW5 T C -61 FW5D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 FW5 T X -61 FW5D_X.gxt RT6U R C -61 RT6U_C.gxt RT6U R X -61 RT6U_X.gxt FW6 T C -61 FW6D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 FW6 T X -61 FW6D_X.gxt

RT7U R C -61 RT7U_C.gxt RT7U R X -61 RT7U_X.gxt FW7 T C -61 FW7D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 FW7 T X -61 FW7D_X.gxt RT8U R C -61 RT8U_C.gxt RT8U R X -61 RT8U_X.gxt FW8 T C -61 FW8D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 FW8 T X -61 FW8D_X.gxt RT9U R C -61 RT9U_C.gxt RT9U R X -61 RT9U_X.gxt FW9 T C -61 FW9D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 FW9 T X -61 FW9D_X.gxt FW1 R C -61 FW1U_C.gxt FW1 R X -61 FW1U_X.gxt RT1D T C -61 RT1D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 RT1D T X -61 RT1D_X.gxt FW6 R C -61 FW6U_C.gxt FW6 R X -61 FW6U_X.gxt RT6D T C -61 RT6D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 RT6D T X -61 RT6D_X.gxt FW2 R C -61 FW2U_C.gxt FW2 R X -61 FW2U_X.gxt RT2D T C -61 RT2D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 RT2D T X -61 RT2D_X.gxt FW9 R C -61 FW9U_C.gxt FW9 R X -61 FW9U_X.gxt RT9D T C -61 RT9D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 RT9D T X -61 RT9D_X.gxt FW7 R C -61 FW7U_C.gxt FW7 R X -61 FW7U_X.gxt RT7D T C -61 RT7D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 RT7D T X -61 RT7D_X.gxt FW8 R C -61 FW8U_C.gxt FW8 R X -61 FW8U_X.gxt RT8D T C -61 RT8D_C.gxt -123.5 -123.5 -123.5 -123.5 -123.5 RT8D T X -61 RT8D_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 (T ID Gain (dB) No. ID No. or C) FWR3U 450000 R 28350 R C FWR3 113.4 FWR3U FW3U FWR3D FW3D FWR5U 450000 R 28350 L C FWR5 113.4 FWR5U FW5U FWR5D FW5D FWR1U 450000 R 28350 R C FWR1 113.4 FWR1U FW1U FWR1D FW1D FWR6U 450000 R 28350 L C FWR6 113.4 FWR6U FW6U FWR6D FW6D FWR2U 450000 R 29750 R C FWR2 113.4 FWR2U FW2U FWR2D FW2D FWR9U 450000 R 29750 L C FWR9 113.4 FWR9U FW9U FWR9D FW9D FWR7U 450000 R 29750 R C FWR7 113.4 FWR7U FW7U FWR7D FW7D FWR8U 450000 R 29750 L C FWR8 113.4 FWR8U FW8U FWR8D FW8D RTN3D 450000 T 18550 L C RTN3 113.4 RTN3U RT3U RTN3D RT3D RTN5D 450000 T 18550 R C RTN5 113.4 RTN5U RT5U RTN5D RT5D RTN1D 450000 T 18550 L C RTN1 113.4 RTN1U RT1U RTN1D RT1D RTN6D 450000 T 18550 R C RTN6 113.4 RTN6U RT6U RTN6D RT6D RTN2D 450000 T 19950 L C RTN2 113.4 RTN2U RT2U RTN2D RT2D RTN9D 450000 T 19950 R C RTN9 113.4 RTN9U RT9U RTN9D RT9D RTN7D 450000 T 19950 L C RTN8 113.4 RTN8U RT8U RTN8D RT8D RTN8D 450000 T 19950 R C RTN7 113.4 RTN7U RT7U RTN7D RT7D FWR3D 450000 T 19950 R C FWR5D 450000 T 19950 L C FWR1D 450000 T 19950 R C FWR6D 450000 T 19950 L C FWR2D 450000 T 19950 R C FWR9D 450000 T 19950 L C FWR7D 450000 T 19950 R C FWR8D 450000 T 19950 R C RTN3U 450000 R 29750 L C RTN5U 450000 R 29750 R C RTN1U 450000 R 29750 L C RTN6U 450000 R 29750 R C RTN2U 450000 R 29750 L C RTN9U 450000 R 29750 R C

RTN7U 450000 R 29750 L C RTN8U 450000 R 29750 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) 1 450MG7W 450000 16 1035750 0.75 10.7 22.9 2 450MG7W 450000 8 779250 0.75 8.3 20.5 3 45M0G7W 45000 16 103575 0.75 10.7 22.9 4 45M0G7W 45000 8 77925 0.75 8.3 20.5 5 5M60G7W 5600 4 8000 0.857 7.5 19.7 6 4M00G7W 4000 8 8000 0.857 11.6 23.8 7 1M00G7W 1000 8 2000 0.857 11.6 23.8 8 1M40G7W 1400 4 2000 0.857 7.5 19.7 9 45M0G7W 45000 8 70687 0.666 7 19.2

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. 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) FWR1 FWR9 1 1 Forward Ka-ban 63 14.6 19.6 64 64 -124.5 23.3 FWR1 FWR9 2 1 Forward Ka-ban 63 15.4 20.4 62.5 64.5 -124 19.5 FWR1 FWR9 3 10 Forward Ka-ban 63 6.1 11.1 52.5 52.5 -126 23.3 FWR1 FWR9 4 10 Forward Ka-ban 63 4.6 9.6 52.5 52.5 -126 19.5 RTN1 RTN9 5 80 return ka 5.pdf 44.9 2.6 7.6 32.2 32.2 -137.3 36.3 RTN1 RTN9 6 112 return ka 6.pdf 46.6 5.6 10.6 37 37 -131 36.3 RTN1 RTN9 7 450 return ka 7.pdf 44.9 1.4 6.4 31 31 -131 36.3 RTN1 RTN9 8 321 return ka 8.pdf 38.9 2.6 7.6 26.2 26.2 -137.3 36.3 FWR1 FWR9 9 10 DTH Ka-band 9 63 6.62 11.62 50.5 52.5 -126 19.5

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 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 2778 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3459 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6254 26.06 0.846 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1057 8.82 0.8863 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 74.2 8.11 0.75 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): 11596 11596 11596 11596 Bus (Watts): (b): (g): (l): (q): 2890 1559 2890 1559 Total (Watts): (c): (h): (m): (r): 14486 13155 14486 13155 Solar Array (Watts): (d): (i): (n): (s): 17537 15678 15865 14331 Depth of Battery (e) (j) (o) (t) Discharge (%): 78.9 % % 78.9 % % 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: 2012-04-24 15:22:58
Document Modified: 2012-04-24 15:22:58
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