Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20040319-00039 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2004031900039_368226

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: AMC-9 6/30/2003 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 20 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 48 0 MHz d. Estimated Launch Date: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply: 6/7/2003 1728 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) 11700 M 12200 M T Direct to Home in the Fixed Fixed Satellite Service 11700 M 12200 M T Fixed Satellite Service 14000 M 14500 M R Direct to Home in the Fixed Fixed Satellite Service 14000 M 14500 M R Fixed Satellite Service 3700 M 4200 M T Direct to Home in the Fixed Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 5925 M 6425 M R Direct to Home in the Fixed Fixed Satellite Service 5925 M 6425 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: 83 W The geostationary arc, for providing domestic service Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be in the C and Ku frequency bands, is heavily used. N/S Station-Keeping provided (Optional): Most orbit locations are already occupied or licensed d. Toward West: Degrees E/W 0.05 Degrees Tolerance: by the FCC. 83° W.L. was selected because it g. Westernmost: W e. Toward East: 0.05 Degrees recently became available for re-assignment, and 0.05 Degrees h. Easternmost: W adequate coverage (e.g., minimum elevation angle) of the desired service areas is possible from this location. 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) CNA E -15 dB gain contour of beams CUH and CUV for the uplink; -10 dB gain contour of beams CDH and CDV for the

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) CDH T 30 20 0.15 0 0 CNA CDV T 30 20 0.15 0 90 CNA CUH R 33.2 18.2 0.15 0 0 CNA CUV R 33.2 18.2 0.15 0 90 CNA KDH T 0.15 0 KDV T 0.15 0 KUH R 0.15 0 KUV R 0.15 0

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) CDH T C -83 83W H 12C EIRP 41_4.gxt -152 -151 -151 -150 -150 CDV T C -83 amc-9 83W V 13C EIRP 41_4 dBW.gxt-152 -151 -151 -150 -150 CUH R C -83 amc-9 83W H 13C G_T 5.gxt CUV R C -83 amc-9 83W V 12C G_T 5 dBK.gxt KUH R C -83 amc-9 83W H 13K G_T 4_8.gxt KUV R C -83 amc-9 83W V 12K G_T 4_8.gxt KDH T C -83 amc-9 83W H 12K EIRP 53_3 dBW.gxt KDV T C -83 amc-9 83W V 13K EIRP 53_3 dBW.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 ID Gain (dB) No. ID No. (T or C) CD007 36000 T 3840 H C C0001 117.4 CU001 CUH CD001 CDV CD009 36000 T 3880 H C C0003 117.4 CU003 CUH CD003 CDV CD011 36000 T 3920 H C C0005 117.4 CU005 CUH CD005 CDV CD013 36000 T 3960 H C C0007 117.4 CU007 CUH CD007 CDV CD015 36000 T 4000 H C C0009 117.4 CU009 CUH CD009 CDV CD017 36000 T 4040 H C C0011 117.4 CU011 CUH CD011 CDV CD019 36000 T 4080 H C C0013 117.4 CU013 CUH CD013 CDV CD021 36000 T 4120 H C C0015 117.4 CU015 CUH CD015 CDV CD023 36000 T 4160 H C C0017 117.4 CU017 CUH CD017 CDV CD002 36000 T 3740 V C C0019 117.4 CU019 CUH CD019 CDV CD004 36000 T 3780 V C C0021 117.4 CU021 CUH CD021 CDV CD006 36000 T 3820 V C C0023 117.4 CU023 CUH CD023 CDV CD008 36000 T 3860 V C C0002 117.4 CU002 CUV CD002 CDH CD010 36000 T 3900 V C C0004 117.4 CU004 CUV CD004 CDH CD012 36000 T 3940 V C C0006 117.4 CU006 CUV CD006 CDH CD014 36000 T 3980 V C C0008 117.4 CU008 CUV CD008 CDH CD016 36000 T 4020 V C C0010 117.4 CU010 CUV CD010 CDH CD018 36000 T 4060 V C C0012 117.4 CU012 CUV CD012 CDH CD020 36000 T 4100 V C C0014 117.4 CU014 CUV CD014 CDH CD022 36000 T 4140 V C C0016 117.4 CU016 CUV CD016 CDH CD024 36000 T 4180 V C C0018 117.4 CU018 CUV CD018 CDH CU001 36000 R 5945 V C C0020 117.4 CU020 CUV CD020 CDH CU003 36000 R 5985 V C C0022 117.4 CU022 CUV CD022 CDH CU005 36000 R 6025 V C C0024 117.4 CU024 CUV CD024 CDH CU007 36000 R 6065 V C K0001 128.5 KU001 KUH KD001 KDV CU009 36000 R 6105 V C K0003 128.5 KU003 KUH KD003 KDV CU011 36000 R 6145 V C K0005 128.5 KU005 KUH KD005 KDV CU013 36000 R 6185 V C K0007 128.5 KU007 KUH KD007 KDV CU015 36000 R 6225 V C K0009 128.5 KU009 KUH KD009 KDV CU017 36000 R 6265 V C K0011 128.5 KU011 KUH KD011 KDV

CU019 36000 R 6305 V C K0013 128.5 KU013 KUH KD013 KDV CU021 36000 R 6345 V C K0015 128.5 KU015 KUH KD015 KDV CU023 36000 R 6385 V C K0017 128.5 KU017 KUH KD017 KDV CU002 36000 R 5965 H C K0019 128.5 KU019 KUH KD019 KDV CU004 36000 R 6005 H C K0021 128.5 KU021 KUH KD021 KDV CU006 36000 R 6045 H C K0023 128.5 KU023 KUH KD023 KDV CU008 36000 R 6085 H C K0002 128.5 KU002 KUV KD002 KDH CU010 36000 R 6125 H C K0004 128.5 KU004 KUV KD004 KDH CU012 36000 R 6165 H C K0006 128.5 KU006 KUV KD006 KDH CU014 36000 R 6205 H C K0008 128.5 KU008 KUV KD008 KDH CU016 36000 R 6245 H C K0010 128.5 KU010 KUV KD010 KDH CU018 36000 R 6285 H C K0012 128.5 KU012 KUV KD012 KDH CU020 36000 R 6325 H C K0014 128.5 KU014 KUV KD014 KDH CU022 36000 R 6365 H C K0016 128.5 KU016 KUV KD016 KDH CU024 36000 R 6405 H C K0018 128.5 KU018 KUV KD018 KDH KD001 36000 T 11720 V C K0020 128.5 KU020 KUV KD020 KDH KD003 36000 T 11760 V C K0022 128.5 KU022 KUV KD022 KDH KD005 36000 T 11800 V C K0024 128.5 KU024 KUV KD024 KDH KD007 36000 T 11840 V C KD009 36000 T 11880 V C KD011 36000 T 11920 V C KD013 36000 T 11960 V C KD015 36000 T 12000 V C KD017 36000 T 12040 V C KD019 36000 T 12080 V C KD021 36000 T 12120 V C KD023 36000 T 12160 V C KD002 36000 T 11740 H C KD004 36000 T 11780 H C KD006 36000 T 11820 H C KD008 36000 T 11860 H C KD010 36000 T 11900 H C KD012 36000 T 11940 H C KD014 36000 T 11980 H C KD016 36000 T 12020 H C KD018 36000 T 12060 H C KD020 36000 T 12100 H C KD022 36000 T 12140 H C KD024 36000 T 12180 H C

KU001 36000 R 14020 H C KU003 36000 R 14060 H C KU005 36000 R 14100 H C KU007 36000 R 14140 H C KU009 36000 R 14180 H C KU011 36000 R 14220 H C KU013 36000 R 14260 H C KU015 36000 R 14300 H C KU017 36000 R 14340 H C KU019 36000 R 14380 H C KU021 36000 R 14420 H C KU023 36000 R 14460 H C KU002 36000 R 14040 V C KU004 36000 R 14080 V C KU006 36000 R 14120 V C KU008 36000 R 14160 V C KU010 36000 R 14200 V C KU012 36000 R 14240 V C KU014 36000 R 14280 V C KU016 36000 R 14320 V C KU018 36000 R 14360 V C KU020 36000 R 14400 V C KU022 36000 R 14440 V C KU024 36000 R 14480 V C CD001 36000 T 3720 H C CD003 36000 T 3760 H C CD005 36000 T 3800 H 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) A 36M0G7W 36000 4 40000 0.691 6.8 19 B 6M95G1W 6950 4 8000 0.691 6.8 19 C 36M0G7W 36000 8 60000 0.614 9.9 22.1 D 36M0G7W 36000 16 110000 0.806 16.6 28.8 E 100KG1W 100 4 56 0.691 6.8 19 F 1M35G7W 1350 4 1544 0.691 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) G 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 12 26

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) C0001 C0024 A 1 17 53.8 7.7 26.7 31.6 41.4 -159.5 22.3 C0001 C0024 B 5 6950 17 53.8 -7.8 11.2 22.7 34.9 -159.7 23.7 C0001 C0024 C 1 19 53.8 7.7 26.7 31.1 41.4 -160 29.8 C0001 C0024 D 1 53.8 7.7 26.7 36.3 41.4 -160.2 29.8 C0001 C0024 E 360 100 47.8 -20 -1.8 3 15.8 -156.5 22.3 C0001 C0024 F 26 1350 47.8 -5.6 13.4 17.8 27.7 -159.6 22.3 K0001 K0024 A 1 57.3 7.2 26 47.7 53.3 -147.6 17.1 K0001 K0024 B 5 6950 53 -3.9 14.9 34.9 46.8 -147.2 25.6 K0001 K0024 C 1 57.3 7.2 26 45.7 53.3 -148.1 25.6 K0001 K0024 D 1 60.7 3.8 22.6 48.6 53.3 -148.3 33.6 K0001 K0024 E 360 100 46.7 -14.8 4 17.5 27.7 -144.6 19.6 K0001 K0024 F 26 1350 46.7 -4.8 14 27.8 39.6 -147.1 25.6 C0001 C0024 G 1 5500 53.2 8.3 27.3 35.3 41.4 -152.3 23.7 C0001 C0001 1 2000 57.2 7.3 26.1 46.1 53.3 -136 29.4

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: Woodbine TT&C S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Mt. Airy MD 21771 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 410-549-4300 E7169 Remote Control (TT C) Location(s): S14a: Street Address: Vernon Valley Spacecraft Ops S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Sussex NJ 07461 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 973-823-6000 WB81 Remote Control (TT C) Location(s): S14a: Street Address: Grand Junction S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Grand Junction CO 81505 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 970-241-8300 E890537 Remote Control (TT C) Location(s): S14a: Street Address: SES Americom S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Somis CA 93066 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 805-386-4195 E940156

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 (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: 6.9 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1.8 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 64.9 3.7 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): 6125 6125 Bus (Watts): (b): (g): (l): (q): 2046 1143 Total (Watts): (c): (h): (m): (r): 8171 7267 Solar Array (Watts): (d): (i): (n): (s): 10744 9608 Depth of Battery (e) (j) (o) (t) Discharge (%): % % % % 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: 2004-04-12 11:11:37
Document Modified: 2004-04-12 11:11:37
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