Attachment Sched S Tech Report

This document pretains to SAT-MOD-20111220-00243 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2011122000243_931061

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-3 9/30/1997 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 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: 9/3/1997 9/3/1997 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 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) 14.00 G 14.50 G R Fixed Satellite Service 11.70 G 12.20 G T Fixed Satellite Service 5.925 G 6.425 G R Fixed Satellite Service 3.70 G 4.20 G T Fixed Satellite Service 11.70 G 12.20 G T Direct to Home in the Fixed Fixed Satellite Service 14.00 G 14.50 G R Direct to Home in the Fixed 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: 67 W Satellite will be colocated with AMC-4 at 67W. Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be N/S Station-Keeping provided (Optional): 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 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) K-DL E Southern US, Mexico, parts of Caribbean K-UL E Southern US, Mexico, parts of Caribbean C-DL E CONUS, Mexico, parts of Central America and Caribbean C-UL E CONUS, Mexico, parts of Central America and Caribbean

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 33 23 0.15 0 30 Y 0 C-UL 537 5.7 -92.4 21 1 CRV R 31.91 21.91 0.15 0 30 Y 90 C-UL 513 4.81 -91.51 21 1 KRH R 35.12 25.12 0.15 0 30 Y 0 K-UL 684 6.77 -93.77 21 1 KRV R 33.93 23.93 0.15 0 30 Y 90 K-UL 714 5.39 -92.39 21 1 CTH T 29.89 19.89 0.15 0 30 Y 0 C-DL 1.8 20 41.1 CTV T 30.67 20.67 0.15 0 30 Y 90 C-DL 1.7 20 42.02 KTH T 33.61 23.61 0.15 0 30 Y 0 K-DL 1 60 50.58 KTV T 33.14 23.14 0.15 0 30 Y 90 K-DL 1 60 50.34

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 -67 CRHclean.gxt CRV R C -67 CRVclean.gxt KRH R C -67 KRHclean.gxt KRV R C -67 KRVclean.gxt CTH T C -67 CTHclean.gxt -166.52 -165.9 -165.05 -164.28 -163.13 CTV T C -67 CTV2clean.gxt -166.52 -165.9 -165.05 -164.28 -163.13 KTH T C -67 KTHclean.gxt KTV T C -67 KTVclean.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) KR01 36000 R 14020 H C K01 120.9 KR01 KRH KT01 KTV KR02 36000 R 14040 V C K03 120.9 KR03 KRH KT03 KTV KR03 36000 R 14060 H C K05 120.9 KR05 KRH KT05 KTV KR04 36000 R 14080 V C K07 120.9 KR07 KRH KT07 KTV KR05 36000 R 14100 H C K09 120.9 KR09 KRH KT09 KTV KR06 36000 R 14120 V C K11 120.9 KR11 KRH KT11 KTV KR07 36000 R 14140 H C K13 120.9 KR13 KRH KT13 KTV KR08 36000 R 14160 V C K15 120.9 KR15 KRH KT15 KTV KR09 36000 R 14180 H C K17 120.9 KR17 KRH KT17 KTV KR10 36000 R 14200 V C K19 120.9 KR19 KRH KT19 KTV KR11 36000 R 14220 H C K21 120.9 KR21 KRH KT21 KTV KR12 36000 R 14240 V C K23 120.9 KR23 KRH KT23 KTV KR13 36000 R 14260 H C K02 120.9 KR02 KRV KT02 KTH KR14 36000 R 14280 V C K04 120.9 KR04 KRV KT04 KTH KR15 36000 R 14300 H C K06 120.9 KR06 KRV KT06 KTH KR16 36000 R 14320 V C K08 120.9 KR08 KRV KT08 KTH KR17 36000 R 14340 H C K10 120.9 KR10 KRV KT10 KTH KR18 36000 R 14360 V C K12 120.9 KR12 KRV KT12 KTH KR19 36000 R 14380 H C K14 120.9 KR14 KRV KT14 KTH KR20 36000 R 14400 V C K16 120.9 KR16 KRV KT16 KTH KR21 36000 R 14420 H C K18 120.9 KR18 KRV KT18 KTH KR22 36000 R 14440 V C K20 120.9 KR20 KRV KT20 KTH KR23 36000 R 14460 H C K22 120.9 KR22 KRV KT22 KTH KR24 36000 R 14480 V C K24 120.9 KR24 KRV KT24 KTH KT01 36000 T 11720 V C C01 109.3 CR01 CRV CT01 CTH KT02 36000 T 11740 H C C03 109.3 CR03 CRV CT03 CTH KT03 36000 T 11760 V C C05 109.3 CR05 CRV CT05 CTH KT04 36000 T 11780 H C C07 109.3 CR07 CRV CT07 CTH KT05 36000 T 11800 V C C09 109.3 CR09 CRV CT09 CTH KT06 36000 T 11820 H C C11 109.3 CR11 CRV CT11 CTH

KT07 36000 T 11840 V C C13 109.3 CR13 CRV CT13 CTH KT08 36000 T 11860 H C C15 109.3 CR15 CRV CT15 CTH KT09 36000 T 11880 V C C17 109.3 CR17 CRV CT17 CTH KT10 36000 T 11900 H C C19 109.3 CR19 CRV CT19 CTH KT11 36000 T 11920 V C C21 109.3 CR21 CRV CT21 CTH KT12 36000 T 11940 H C C23 109.3 CR23 CRV CT23 CTH KT13 36000 T 11960 V C C02 109.3 CR02 CRH CT02 CTV KT14 36000 T 11980 H C C04 109.3 CR04 CRH CT04 CTV KT15 36000 T 12000 V C C06 109.3 CR06 CRH CT06 CTV KT16 36000 T 12020 H C C08 109.3 CR08 CRH CT08 CTV KT17 36000 T 12040 V C C10 109.3 CR10 CRH CT10 CTV KT18 36000 T 12060 H C C12 109.3 CR12 CRH CT12 CTV KT19 36000 T 12080 V C C14 109.3 CR14 CRH CT14 CTV KT20 36000 T 12100 H C C16 109.3 CR16 CRH CT16 CTV KT21 36000 T 12120 V C C18 109.3 CR18 CRH CT18 CTV KT22 36000 T 12140 H C C20 109.3 CR20 CRH CT20 CTV KT23 36000 T 12160 V C C22 109.3 CR22 CRH CT22 CTV KT24 36000 T 12180 H C C24 109.3 CR24 CRH CT24 CTV CR01 36000 R 5945 V C TCC CC1 CRH CR02 36000 R 5965 H C TBC1 CBCN1 CTV CR03 36000 R 5985 V C TBC2 CBCN2 CTH CR04 36000 R 6005 H C TBK2 KBCN2 KTV CR05 36000 R 6025 V C CR06 36000 R 6045 H C CR07 36000 R 6065 V C CR08 36000 R 6085 H C CR09 36000 R 6105 V C CR10 36000 R 6125 H C CR11 36000 R 6145 V C CR12 36000 R 6165 H C CR13 36000 R 6185 V C CR14 36000 R 6205 H C CR15 36000 R 6225 V C CR16 36000 R 6245 H C CR17 36000 R 6265 V C CR18 36000 R 6285 H C CR19 36000 R 6305 V C CR20 36000 R 6325 H C CR21 36000 R 6345 V C

CR22 36000 R 6365 H C CR23 36000 R 6385 V C CR24 36000 R 6405 H C CT01 36000 T 3720 H C CT02 36000 T 3740 V C CT03 36000 T 3760 H C CT04 36000 T 3780 V C CT05 36000 T 3800 H C CT06 36000 T 3820 V C CT07 36000 T 3840 H C CT08 36000 T 3860 V C CT09 36000 T 3880 H C CT10 36000 T 3900 V C CT11 36000 T 3920 H C CT12 36000 T 3940 V C CT13 36000 T 3960 H C CT14 36000 T 3980 V C CT15 36000 T 4000 H C CT16 36000 T 4020 V C CT17 36000 T 4040 H C CT18 36000 T 4060 V C CT19 36000 T 4080 H C CT20 36000 T 4100 V C CT21 36000 T 4120 H C CT22 36000 T 4140 V C CT23 36000 T 4160 H C CT24 36000 T 4180 V C CC1 800 R 6423.5 V T CBCN1 400 T 3700.5 V T CBCN2 400 T 4199.5 H T KBCN2 400 T 12198 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) K_A 36M0G7W 36000 4 40000 0.69 6.8 19 K_B 27M0G7W 27000 4 32000 0.69 6.8 19 K_C 6M95G1W 6950 4 8000 0.69 6.8 19 K_D 5M00G1W 5000 4 6000 0.69 6.8 19 K_E 100KG1W 100 4 56 0.69 6.8 19 K_F 1M60G1W 1600 4 1544 0.69 6.8 19 K_G 36M0G7W 36000 8 50000 0.61 9.9 20 C_A 36M0G7W 36000 4 40000 0.69 6.8 19 C_B 27M0G7W 27000 4 32000 0.69 6.8 19 C_C 6M95G1W 6950 4 8000 0.69 6.8 19 C_D 5M00G1W 5000 4 6000 0.69 6.8 19 C_E 100KG1W 100 4 56 0.69 6.8 19 C_F 1M60G1W 1600 4 1544 0.69 6.8 19 C_G 36M0G7W 36000 8 50000 0.61 9.9 20

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) K_H 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 20 C_H 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 20 K_TM 400KF9D 400 10 20 C_TC 800KF9D 800 10 20 C_TM 400KF9D 400 10 20

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) K01 K24 K_A 1 amc3_S13_link 57.3 15 20 43.5 48.5 -153 20.9 K01 K24 K_B 1 amc3_S13_link 57.3 15 20 42.3 47.3 -153 20.9 K01 K24 K_C 5 6950 amc3_S13_link 53 3.9 8.9 32.4 37.4 -157 26.9 K01 K24 K_D 6 5000 amc3_S13_link 53 3.9 8.9 30.9 35.9 -157 26.9 K01 K24 K_E 250 100 amc3_S13_link 46.7 -8 -2 13.9 18.9 -157 20.9 K01 K24 K_F 20 1544 amc3_S13_link 46.7 3 8 26 31 -157 26.9 K01 K24 K_G 1 amc3_S13_link 57.3 15 20 39.5 44.5 -157 26.9 C01 C24 C_A 1 amc3_S13_link 53.5 20.1 25.1 32 37 -164.5 22.1 C01 C24 C_B 1 amc3_S13_link 53.5 15 20 30.8 35.8 -164.5 22.1 C01 C24 C_C 5 6950 amc3_S13_link 53.5 4.6 9.6 20.9 25.9 -168.5 22.1 C01 C24 C_D 6 5000 amc3_S13_link 53.5 7 12 19.4 24.4 -168.5 22.1 C01 C24 C_E 250 100 amc3_S13_link 47.5 -8.4 -3.4 2.4 7.4 -168.5 22.1 C01 C24 C_F 20 1544 amc3_S13_link 47.5 6.8 11.8 14.5 19.5 -168.5 22.1 C01 C24 C_G 1 amc3_S13_link 53.5 20.1 25.1 28 33 -168.5 22.1 K01 K24 K_H 1 amc3_S13_link 2000 57.3 14 19 43.2 48.2 -140.8 20.9 C01 C24 C_H 1 amc3_S13_link 2000 53.5 20 25 34.7 39.7 -149.3 22.1 TCC TCC C_TC 1 amc3_S13_link 57 5 10 TBC1 TBC2 C_TM 1 amc3_S13_link 16 26 -167 22.5

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: 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 E2037 Remote Control (TT C) Location(s): S14a: Street Address: South Mountain Earth Station S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Somis CA 93066 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 805-386-2710 E000289

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 1310.8 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1338.3 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2649 26.8 0.78 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 320 1.8 0.88 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 75.5 3.78 0.69 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): 3772 3740 3772 3740 Bus (Watts): (b): (g): (l): (q): 1089 674 1089 674 Total (Watts): (c): (h): (m): (r): 4861 4414 4861 4414 Solar Array (Watts): (d): (i): (n): (s): 6513 6212 5250 4836 Depth of Battery (e) (j) (o) (t) Discharge (%): 70 % 70 % 70 % 70 % 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: 2011-12-22 12:58:38
Document Modified: 2011-12-22 12:58:38
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