Attachment Sched S Tech Report.

This document pretains to SES-LIC-20140423-00311 for License on a Satellite Earth Station filing.

IBFS_SESLIC2014042300311_1044613

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: EUTELSAT 65 WEST A 6/30/2016 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 6/30/2013 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 1/31/2016 34 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: 3/1/2016 4/30/2016 18000 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) 27500 M 29000 M R Fixed Satellite Service 29500 M 30000 M R Fixed Satellite Service 18300 M 18800 M T Fixed Satellite Service 19700 M 20200 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: 65.2 W Planned satellite that is the responsibility of another Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be satellite operator and ITU administration. N/S Station-Keeping provided (Optional): d. Toward West: Degrees E/W 0.1 Degrees Tolerance: g. Westernmost: e. Toward East: 0.1 Degrees 0.1 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 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) SA1 S Riverside, CA (Longitude 117.089 degW, Latitude 33.796 degN) SA2 S Cheyenne, WY (Longitude 104.737 degW, Latitude 41.132 degN) SA3 S Germantown, MD (Longitude 77.245 degW, Latitude 39.179 degN)

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) GR1 R 52.7 51.7 0.05 1 21 N SA1 2345 18 -110 25 1 GR2 R 52.7 51.7 0.05 1 21 N SA2 2139 18.4 -110.4 25 1 GR3 R 52.7 51.7 0.05 1 21 N SA3 1951 18.8 -110.8 25 1 GT1 T 49 48 0.05 1 24 N SA1 2.2 160 71 GT2 T 49 48 0.05 1 24 N SA2 2.2 160 71 GT3 T 49 48 0.05 1 24 N SA3 2.2 160 71

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) GR1 R C -65 GR1.gxt GR2 R C -65 GR2.gxt GR3 R C -65 GR3.gxt GT1 T C -65 GT1.gxt -137.3 -132.2 -126 -121.3 -121.2 GT2 T C -65 GT2.gxt -142.3 -142.2 -142 -127.9 -121.2 GT3 T C -65 GT3.gxt -142.3 -142.2 -142 -141.9 -121.2

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) GU1 1000000 R 28000 R C FG1CA GU1 GR1 GU2 1000000 R 28000 L C FG1CB GU2 GR1 GU3 500000 R 28750 R C FG1CC GU3 GR1 GU4 500000 R 28750 L C FG1CD GU4 GR1 GU5 500000 R 29750 R C FG1CE GU5 GR1 GU6 500000 R 29750 L C FG1CF GU6 GR1 GD1 500000 T 18550 L C FG2CA GU1 GR2 GD2 500000 T 18550 R C FG2CB GU2 GR2 GD3 250000 T 19825 L C FG2CC GU3 GR2 GD4 250000 T 20075 L C FG2CD GU4 GR2 GD5A 500000 T 19950 R C FG2CE GU5 GR2 GD5B 250000 T 19825 R C FG2CF GU6 GR2 GD5C 250000 T 20075 R C FG3CA GU1 GR3 FG3CB GU2 GR3 FG3CC GU3 GR3 FG3CD GU4 GR3 FG3CE GU5 GR3 FG3CF GU6 GR3 RG1CA GD1 GT1 RG1CB GD2 GT1 RG1CC GD3 GT1 RG1CD GD4 GT1 RG1CE GD5A GT1 RG2CA GD1 GT2 RG2CB GD2 GT2 RG2CC GD3 GT2 RG2CD GD4 GT2 RG2CE GD5A GT2 RG3CA GD1 GT3 RG3CB GD2 GT3

RG3CC GD3 GT3 RG3CD GD4 GT3 RG3CF GD5B GT3 RG3CG GD5C GT3

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 250MG7W 250000 16 533000 0.6642 9.3 21.5 D2 250MG7W 250000 8 450000 0.747 8.2 20.4 D3 250MG7W 250000 4 358000 0.895 6.6 18.8 D4 3M67G7W 3672 8 6666 0.747 8.2 20.4 D5 1M22G7W 1224 8 1950 0.6642 7.1 19.3 D6 612KG7W 612 4 868 0.8869 6.5 18.7 D7 612KG7W 612 2 243 0.5 -1.3 10.9 D8 40M0G7W 40000 16 85280 0.6642 9.3 21.5 D9 40M0G7W 40000 8 72000 0.747 8.2 20.4 D10 40M0G7W 40000 4 57280 0.895 6.6 18.8

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) FG1CA FG3CF D1 1 LB1.xls 68.8 4.2 17 FG1CA FG3CF D2 1 LB2.xls 68.8 4.2 17 FG1CA FG3CF D3 1 LB3.xls 68.8 4.2 17 RG1CA RG3CG D4 68 LB4.xls 26.6 46.6 -121.2 37.6 RG1CA RG3CG D5 204 LB5.xls 21.9 41.9 -121.2 37.6 RG1CA RG3CG D6 408 LB6.xls 18.9 38.9 -121.2 37.6 RG1CA RG3CG D7 408 LB7.xls 18.9 38.9 -121.2 37.6 FG1CA FG3CF D8 6 LB8.xls 68.8 -3.7 17 FG1CA FG3CF D9 6 LB9.xls 68.8 -3.7 17 FG1CA FG3CF D10 6 LB10.xls 68.8 -3.7 17

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

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 2817 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 94 S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: 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? 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: 2014-04-28 16:16:58
Document Modified: 2014-04-28 16:16:58
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC