Attachment Sched S Tech Report

This document pretains to SAT-PPL-20121018-00183 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2012101800183_973890

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: 35 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 1530 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) 5850 M 6425 M R Fixed Satellite Service 3625 M 4200 M T Fixed Satellite Service 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 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) for 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 for the C and Ku band, we are only seeking authority 0.07 Degrees h. Easternmost: to provide service with AMAZONAS-3 to the U.S. territories in the standard bands (3700-4200 MHz, i. Reason for service are selection (Optional): 5925-6425 MHz, 14-14.5 GHz and 11.7-12.2 GHz); we are not seeking authority to provide service to the U.S.

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 Vsa__va.GXT 01 2 S vupku_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) 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 0.5 CRV R 25.5 15.5 0.05 0.05 30 N 90 1 446 -1 -97 20 0.5 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 KUR R 31 23 0.05 0.05 30 N 02 428 4.7 -94 20 1 KUR R 31 23 0.05 0.05 30 N 90 2 428 4.7 -94 20 1 KUT T 29.9 21.9 0.05 0.05 30 N 02 1.9 18.1 48 KUTV T 29.9 21.9 0.05 0.05 30 N 90 2 1.9 18.1 48

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 VUPCBRAh.GXT CRH R X -61 VUPCBRhX.GXT CTH T C -61 VDWCBRhC.GXT -159.7 -159.7 -159.7 -159.7 -159.7 CTH T X -61 VDWCBRhX.GXT CRV R C -61 VUPCBRAv.GXT CRV R X -61 VUPCBRvX.GXT CTV T C -61 VDWCBRvC.GXT -159.7 -159.7 -159.7 -159.7 -159.7 CTV T X -61 VDWCBRvX.GXT KUR R C -61 vupkunach.GXT KUR R X -61 VUPKUNAXh.GXT KUT T C -61 vdwkunach.GXT -132.5 -132.5 -132.5 -132.5 -132.5 KUT T X -61 VDWKUNAXh.GXT KUR R C -61 vupkunacv.GXT KUR R X -61 VUPKUNAXv.GXT KUTV T C -61 vdwkunacv.GXT -132.5 -132.5 -132.5 -132.5 -132.5 KUTV T X -61 VDWKUNAXv.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 3661 V C 1 124.2 CR1 CRH CT1 CTV CT2 54000 T 3722 V C 2 124.2 CR2 CRH CT2 CTV CT3 54000 T 3783 V C 3 124.2 CR3 CRH CT3 CTV CT4 54000 T 3844 V C 4 124.2 CR4 CRH CT4 CTV CT5 54000 T 3905 V C 5 124.2 CR5 CRH CT5 CTV CT6 54000 T 3966 V C 6 124.2 CR6 CRH CT6 CTV CT7 54000 T 4027 V C 7 124.2 CR7 CRH CT7 CTV CT8 54000 T 4088 V C 8 124.2 CR8 CRH CT8 CTV CT9 36000 T 4140 V C 9 124.2 CR9 CRH CT9 CTV CT10 36000 T 4180 V C 10 124.2 CR10 CRH CT10 CTV CT11 54000 T 3652 H C 11 124.2 CR11 CRV CT11 CTH CT12 54000 T 3713 H C 12 124.2 CR12 CRV CT12 CTH CT13 54000 T 3774 H C 13 124.2 CR13 CRV CT13 CTH CT14 54000 T 3835 H C 14 124.2 CR14 CRV CT14 CTH CT15 54000 T 3896 H C 15 124.2 CR15 CRV CT15 CTH CT16 54000 T 3970 H C 16 124.2 CR16 CRV CT16 CTH CT17 54000 T 4031 H C 17 124.2 CR17 CRV CT17 CTH CT18 54000 T 4092 H C 18 124.2 CR18 CRV CT18 CTH CT19 54000 T 4153 H C 19 124.2 CR19 CRV CT19 CTH CR1 54000 R 5886 H C 20 127.1 KR1 KURH KT1 KUTV CR2 54000 R 5947 H C 21 127.1 KR2 KURH KT2 KUTV CR3 54000 R 6008 H C 22 127.1 KR3 KURV KT3 KUTH CR4 54000 R 6069 H C 23 127.1 KR4 KURV KT4 KUTH CR5 54000 R 6130 H C 24 127.1 KR5 KURH KT5 KUTV CR6 54000 R 6191 H C 25 127.1 KR6 KURH KT6 KUTV CR7 54000 R 6252 H C 26 127.1 KR7 KURH KT7 KUTV CR8 54000 R 6313 H C 27 127.1 KR8 KURH KT8 KUTV CR9 36000 R 6365 H C 28 127.1 KR9 KURH KT9 KUTV CR10 36000 R 6405 H C 29 127.1 KR10 KURH KT10 KUTV CR11 54000 R 5877 V C 30 127.1 KR11 KURV KT11 KUTH

CR12 54000 R 5938 V C 31 127.1 KR12 KURV KT12 KUTH CR13 54000 R 5999 V C 32 127.1 KR13 KURV KT13 KUTH CR14 54000 R 6060 V C 33 127.1 KR14 KURV KT14 KUTH CR15 54000 R 6121 V C 34 127.1 KR15 KURV KT15 KUTH CR16 54000 R 6195 V C 35 127.1 KR16 KURV KT16 KUTH CR17 54000 R 6256 V C CR18 54000 R 6317 V C CR19 54000 R 6378 V C KT1 54000 T 11738 V C KT2 54000 T 11799 V C KT3 54000 T 11738 H C KT4 54000 T 11799 H C KT5 36000 T 11972 V C KT6 36000 T 12012 V C KT7 36000 T 12052 V C KT8 36000 T 12092 V C KT9 36000 T 12132 V C KT10 36000 T 12172 V C KT11 36000 T 11972 H C KT12 36000 T 12012 H C KT13 36000 T 12052 H C KT14 36000 T 12092 H C KT15 36000 T 12132 H C KT16 36000 T 12172 H C KR1 54000 R 14034 H C KR2 54000 R 14095 H C KR3 54000 R 14034 V C KR4 54000 R 14095 V C KR5 36000 R 13772 H C KR6 36000 R 13812 H C KR7 36000 R 13852 H C KR8 36000 R 13892 H C KR9 36000 R 13932 H C KR10 36000 R 13972 H C KR11 36000 R 13772 V C KR12 36000 R 13812 V C KR13 36000 R 13852 V C KR14 36000 R 13892 V C KR15 36000 R 13932 V C

KR16 36000 R 13972 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 70K0G7W 70 8 64 0.66666667 8 20.2 2 1M70G7W 1700 8 2048 0.66666667 8 20.2 3 7M50G7W 7500 4 8448 0.75 9 21.2 4 36M0G7W 36000 4 45000 0.875 7.4 19.6 5 1M80G7W 1800 4 2048 0.75 9 17.7 6 36M0G7W 36000 4 38010 0.75 6.1 18.3 7 9M00G7W 9000 8 11300 0.66666667 8 20.2 8 14K0G7W 14 4 11000 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. 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) 1 8 1 800 Link_Budget_1. 47 -5 2 4.5 9.5 -164.5 24.5 1 19 1 318 Link_Budget_2. 47 -1 6 8.7 13.7 -160.4 18.9 1 8 2 30 Link_Budget_3. 47 9.2 16.2 18.9 23.9 -163.3 24.5 1 19 2 10 Link_Budget_4. 47 14 21 23.6 28.6 -159.7 18.9 1 8 3 5 Link_Budget_5. 47 17 24 26.6 31.6 -163.2 24.5 1 19 4 1 Link_Budget_6. 47 20 27 29.7 34.7 -166.9 30 9 10 1 800 Link_Budget_1. 47 -5 2 4.5 9.5 -164.5 24.5 11 19 1 800 Link_Budget_1. 47 -5 2 4.5 9.5 -164.5 24.5 9 10 2 30 Link_Budget_3. 47 9.2 16.2 18.9 23.9 -163.3 24.5 11 19 2 30 Link_Budget_3. 47 9.2 16.2 18.9 23.9 -163.3 24.5 9 10 3 5 Link_Budget_5. 47 17 24 26.6 31.6 -163.2 24.5 11 19 3 5 Link_Budget_5. 47 17 24 26.6 31.6 -163.2 24.5 20 35 5 18 Link_Budget_7. 53 2.5 9.5 27.1 32.1 -132.5 30 20 23 8 2340 Link_Budget_8. 43 -15 -8 2.6 5.6 -137.8 31 24 35 8 2340 Link_Budget_8. 43 -15 -8 2.6 5.6 -137.8 31 20 23 8 2340 Link_Budget_9. 49.2 -16.4 -9.4 5.4 10.4 -133 26.3 24 35 8 2340 Link_Budget_9. 49.2 -16.4 -9.4 5.4 10.4 -133 26.3 20 35 6 1 Link_Budget_1 53 16 23 40.1 45.1 -132.5 26.3 20 35 7 4 Link_Budget_1 53 8.1 15.1 32.7 37.7 -134 30

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 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: 2012-11-06 12:05:30
Document Modified: 2012-11-06 12:05:30
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