Attachment Sched S Tech Report

This document pretains to SAT-AMD-20100302-00038 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2010030200038_804720

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: GALAXY KA N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 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: 880 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) 29500 M 30000 M R Fixed Satellite Service 19700 M 20200 M T Fixed Satellite Service 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 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: 89.1 W PROVIDE KA-BAND SERVICE TO THE Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be CONTINENTAL UNITED STATES, HAWAII, PUERTO N/S Station-Keeping provided (Optional): RICO AND PORTIONS OF ALASKA d. Toward West: Degrees E/W 0.05 Degrees Tolerance: g. Westernmost: e. Toward East: 0.05 Degrees 0.05 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 CONTINENTAL UNITED STATES, HAWAII, PUERTO RICO AND PORTIONS OF ALASKA 2 S GLOBAL

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) NRF R 35.5 31.5 0.11 0.11 30 N 1 795 6.5 -98.2 25 1 NRFL R 35.5 31.5 0.11 0.11 30 N 1 795 6.5 -98.2 25 1 NTF T 35 31 0.11 0.11 30 N 1 1 416.9 61.2 NTFL T 35 31 0.11 0.11 30 N 1 1 416.9 61.2 CMD R 35.5 25.5 0.11 0.11 N 1 5157 -1.6 -115 CMD R 13.2 10.2 0.11 0.11 N 2 917 -16.4 -100.2 CMD R 2.2 -0.8 0.11 0.11 N 02 2011 -30.8 -91.8 TLM T 35 25 0.11 0.11 N 1 1.5 0.28 29.5 TLM T 13.2 10.2 0.11 0.11 N 2 1.5 21.4 26.5 TLM T 2.7 -0.3 0.11 0.11 N 02 1.1 7.8 11.6 ULP T 20.2 17.6 0.11 0.11 N 90 2 1 0.32 15.2

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) NRF R C -89.1 nrfr.gxt NRFL R C -89.1 nrfl.gxt NTF T C -89.1 ntfr.gxt -119.2 -119.1 -119 -118.8 -118.7 NTFL T C -89.1 ntfl.gxt -119.2 -119.1 -119 -118.8 -118.7 CMD R C -89.1 cmdc.gxt CMD R C -89.1 cmdb.pdf TLM T C -89.1 tlmc.gxt -127.8 -127.6 -127.5 -127.4 -127.3 TLM T C -89.1 tlmw.pdf -130.8 -130.6 -130.5 -130.4 -130.3 TLM T C -89.1 tlmb.pdf -169.6 -169.5 -169.4 -169.3 -169.2 ULP T C -89.1 ulpc.gxt -132.1 -131.9 -131.8 -131.7 -131.6 CMD R C -89.1 cmdw.pdf

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) NR001 110000 R 29561 R C N0001 139.8 NR001 NRFR NT001 NTFL NR003 110000 R 29683 R C N0003 139.8 NR003 NRFR NT003 NTFL NR005 110000 R 29805 R C N0005 139.8 NR005 NRFR NT005 NTFL NR007 110000 R 29927 R C N0007 139.8 NR007 NRFR NT007 NTFL NR002 110000 R 29561 L C N0002 139.8 NR002 NRFL NT002 NTFR NR004 110000 R 29683 L C N0004 139.8 NR004 NRFL NT004 NTFR NR006 110000 R 29805 L C N0006 139.8 NR006 NRFL NT006 NTFR NR008 110000 R 29927 L C N0008 139.8 NR008 NRFL NT008 NTFR NT001 110000 T 19761 L C NT003 110000 T 19883 L C NT005 110000 T 20005 L C NT007 110000 T 20127 L C NT002 110000 T 19761 R C NT004 110000 T 19883 R C NT006 110000 T 20005 R C NT008 110000 T 20127 R C CMD1 1000 R 29996 R T CMD2 1000 R 29998 L T CMD3 1000 R 6422 H T TLM1 500 T 20195.5 R T TLM2 500 T 20196.5 R T TLM3 500 T 20195.5 L T TLM4 500 T 20196.5 L T TLM5 500 T 4198.75 H T TLM6 500 T 4199.25 H T UPC1 25 T 20199.5 V T

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 110MG7W 110000 4 86270 0.5 3.1 10.4 D2 10M3G7W 10300 4 6240 0.5 3.9 10.7 D3 100KG7W 100 4 70 0.5 3 9.5 D4 1M45G7W 1450 2 610 0.5 3.4 10.5 D5 400KG7W 400 2 150 0.5 3.4 21.5

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) N0001 N0008 D1 1 LINK BUDGET 63.6 17.7 21.7 57.2 61.2 -120.6 18.6 N0001 N0008 D2 7 10300 NOTE.txt 63.6 1.8 5.8 48.4 52.4 -118 18.1 N0001 N0008 D3 689 100 NOTE.txt 63.6 -17.8 -13.8 28.8 32.8 -118 17.8 N0001 N0008 D4 74 1450 NOTE.txt 63.6 -8.1 -4.1 38.5 42.5 -120.5 18.6 N0001 N0008 D5 275 400 NOTE.txt 44.4 -5.8 -1.8 21.7 25.7 -131.2 37.8

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: 3400 INTERNATIONAL DRIVE, N.W. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: WASHINGTON DC 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202-944-7701

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 2181 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2399 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4580 24.8 0.882 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 633 6.4 0.858 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 86.7 6.4 0.757 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): 7538 7538 7538 7538 Bus (Watts): (b): (g): (l): (q): 1508 1508 1508 1508 Total (Watts): (c): (h): (m): (r): 9046 9046 9046 9046 Solar Array (Watts): (d): (i): (n): (s): 12149 10945 11045 9950 Depth of Battery (e) (j) (o) (t) Discharge (%): 73.2 % % 76.3 % % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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: 2010-03-03 09:21:27
Document Modified: 2010-03-03 09:21:27
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