Attachment Sched S Tech Report

This document pretains to SAT-MOD-20100324-00056 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2010032400056_807501

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-2 3/5/1997 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/1/1994 14.8 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 8/1/1996 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: 1/30/1997 1/30/1997 1920 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) 14.0 G 14.5 G R Fixed Satellite Service 14.0 G 14.5 G R Direct to Home in the Fixed Fixed Satellite Service 11.7 G 12.20 G T Fixed Satellite Service 11.7 G 12.2 G T Direct to Home in the Fixed Fixed Satellite Service 5.925 G 6.425 G R Fixed Satellite Service 3.7 G 4.2 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: 78.95 W To replace AMC-5 and Satcom C3 at the nominal 79W Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be orbital location. 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 (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) KUL E US CONUS and partial Caribbean coverage, -6 dB contour KDL E US CONUS and partial Caribbean coverage, -6 dB contour CUL E US CONUS and Caribbean coverage, -6 dB contour CDL E US CONUS and Caribbean coverage, -6 dB contour GBL E Global region for TT&C

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) KRV R 30.86 24.86 0.15 0 30 Y 90 KUL 550 3.46 -96.5 18 1 KRH R 33.63 27.63 0.15 0 30 Y 0 KUL 590 5.93 -99 18 1 KTV T 33 27 0.15 0 30 Y 90 KDL 1.5 41.7 49.2 KTH T 33.27 27.27 0.15 0 30 Y 0 KDL 1.4 43.7 49.68 CRV R 32.38 23.38 0.15 0 30 Y 90 CUL 605 4.48 -100 18 1 CRH R 32.86 23.86 0.15 0 30 Y 0 CUL 540 5.56 -101 18 1 CTV T 30.58 21.58 0.15 0 30 Y 90 CDL 1.9 12.9 41.69 CTH T 31.48 22.48 0.15 0 30 Y 0 CDL 2.5 11.2 41.98 GBL R 10 0.15 0 30 Y 90 GBL 600 -7 GBL R 10 0.15 0 30 Y 0 GBL 600 -7

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) KRV R C -78.95 KRV.gxt KRH R C -78.95 KRH.gxt CRV R C -78.95 CRV.gxt CRH R C -78.95 CRH.gxt KTV T C -78.95 KTV.gxt KTH T C -78.95 KTH.gxt CTV T C -78.95 CTV.gxt -155.5 -154.8 -154.3 -153.8 -153.6 CTH T C -78.95 CTH.gxt -153.6 -153.4 -153 -152.5 -152.1 GBL R C -78.95 GBL R C -78.95

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) KR001 36000 R 14020 V C K0001 120 KR001 KRV KT001 KTH KR002 36000 R 14040 H C K0002 120 KR002 KRH KT002 KTV KR003 36000 R 14060 V C K0003 120 KR003 KRV KT003 KTH KR004 36000 R 14080 H C K0004 120 KR004 KRH KT004 KTV KR005 36000 R 14100 V C K0005 120 KR005 KRV KT005 KTH KR006 36000 R 14120 H C K0006 120 KR006 KRH KT006 KTV KR007 36000 R 14140 V C K0007 120 KR007 KRV KT007 KTH KR008 36000 R 14160 H C K0008 120 KR008 KRH KT008 KTV KR009 36000 R 14180 V C K0009 120 KR009 KRV KT009 KTH KR010 36000 R 14200 H C K0010 120 KR010 KRH KT010 KTV KR011 36000 R 14220 V C K0011 120 KR011 KRV KT011 KTH KR012 36000 R 14240 H C K0012 120 KR012 KRH KT012 KTV KR013 36000 R 14260 V C K0013 120 KR013 KRV KT013 KTH KR014 36000 R 14280 H C K0014 120 KR014 KRH KT014 KTV KR015 36000 R 14300 V C K0015 120 KR015 KRV KT015 KTH KR016 36000 R 14320 H C K0016 120 KR016 KRH KT016 KTV KR017 36000 R 14340 V C K0017 120 KR017 KRV KT017 KTH KR018 36000 R 14360 H C K0018 120 KR018 KRH KT018 KTV KR019 36000 R 14380 V C K0019 120 KR019 KRV KT019 KTH KR020 36000 R 14400 H C K0020 120 KR020 KRH KT020 KTV KR021 36000 R 14420 V C K0021 120 KR021 KRV KT021 KTH KR022 36000 R 14440 H C K0022 120 KR022 KRH KT022 KTV KR023 36000 R 14460 V C K0023 120 KR023 KRV KT023 KTH KR024 36000 R 14480 H C K0024 120 KR024 KRH KT024 KTV KT001 36000 T 11720 H C C0001 109 CR001 CRV CT001 CTH KT002 36000 T 11740 V C C0002 109 CR002 CRH CT002 CTV KT003 36000 T 11760 H C C0003 109 CR003 CRV CT003 CTH KT004 36000 T 11780 V C C0004 109 CR004 CRH CT004 CTV KT005 36000 T 11800 H C C0005 109 CR005 CRV CT005 CTH KT006 36000 T 11820 V C C0006 109 CR006 CRH CT006 CTV

KT007 36000 T 11840 H C C0007 109 CR007 CRV CT007 CTH KT008 36000 T 11860 V C C0008 109 CR008 CRH CT008 CTV KT009 36000 T 11880 H C C0009 109 CR009 CRV CT009 CTH KT010 36000 T 11900 V C C0010 109 CR010 CRH CT010 CTV KT011 36000 T 11920 H C C0011 109 CR011 CRV CT011 CTH KT012 36000 T 11940 V C C0012 109 CR012 CRH CT012 CTV KT013 36000 T 11960 H C C0013 109 CR013 CRV CT013 CTH KT014 36000 T 11980 V C C0014 109 CR014 CRH CT014 CTV KT015 36000 T 12000 H C C0015 109 CR015 CRV CT015 CTH KT016 36000 T 12020 V C C0016 109 CR016 CRH CT016 CTV KT017 36000 T 12040 H C C0017 109 CR017 CRV CT017 CTH KT018 36000 T 12060 V C C0018 109 CR018 CRH CT018 CTV KT019 36000 T 12080 H C C0019 109 CR019 CRV CT019 CTH KT020 36000 T 12100 V C C0020 109 CR020 CRH CT020 CTV KT021 36000 T 12120 H C C0021 109 CR021 CRV CT021 CTH KT022 36000 T 12140 V C C0022 109 CR022 CRH CT022 CTV KT023 36000 T 12160 H C C0023 109 CR023 CRV CT023 CTH KT024 36000 T 12180 V C C0024 109 CR024 CRH CT024 CTV CR001 36000 R 5945 V C C1 TC GBLRH CR002 36000 R 5965 H C T1 TM1 CTV CR003 36000 R 5985 V C T2 TM2 CTH CR004 36000 R 6005 H C T3 TM3 KTH CR005 36000 R 6025 V C CR006 36000 R 6045 H C CR007 36000 R 6065 V C CR008 36000 R 6085 H C CR009 36000 R 6105 V C CR010 36000 R 6125 H C CR011 36000 R 6145 V C CR012 36000 R 6165 H C CR013 36000 R 6185 V C CR014 36000 R 6205 H C CR015 36000 R 6225 V C CR016 36000 R 6245 H C CR017 36000 R 6265 V C CR018 36000 R 6285 H C CR019 36000 R 6305 V C CR020 36000 R 6325 H C CR021 36000 R 6345 V C

CR022 36000 R 6365 H C CR023 36000 R 6385 V C CR024 36000 R 6405 H C CT001 36000 T 3720 H C CT002 36000 T 3740 V C CT003 36000 T 3760 H C CT004 36000 T 3780 V C CT005 36000 T 3800 H C CT006 36000 T 3820 V C CT007 36000 T 3840 H C CT008 36000 T 3860 V C CT009 36000 T 3880 H C CT010 36000 T 3900 V C CT011 36000 T 3920 H C CT012 36000 T 3940 V C CT013 36000 T 3960 H C CT014 36000 T 3980 V C CT015 36000 T 4000 H C CT016 36000 T 4020 V C CT017 36000 T 4040 H C CT018 36000 T 4060 V C CT019 36000 T 4080 H C CT020 36000 T 4100 V C CT021 36000 T 4120 H C CT022 36000 T 4140 V C CT023 36000 T 4160 H C CT024 36000 T 4180 V C TC 800 R 6423.5 V T TM1 300 T 3700.5 V T TM2 300 T 4199.5 H T TM3 300 T 12198.0 H 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) A_KU 36M0G7W 36000 4 40000 0.69 6.4 18 B_KU 27M0G7W 27000 4 32000 0.69 6.4 18 C_KU 6M95G1W 6950 4 8000 0.69 6.4 18 D_KU 5M00G1W 5000 4 6000 0.69 6.4 18 E_KU 100KG1W 100 4 56 0.69 6.4 18 F_KU 1M60G1W 1600 4 1544 0.69 6.4 18 G_KU 36M7W 36000 8 50000 0.61 9.9 20 H_C 36M0G7W 36000 4 40000 0.59 6.8 18 I_C 6M95G1W 6950 4 8000 0.69 6.8 18 J_C 36M0G7W 36000 8 60000 0.61 9.9 22 K_C 36M0G7W 36000 16 110000 0.81 16.6 24 L_C 100KG1D 100 4 56 0.75 7.2 18 M_C 1M60G1D 1600 4 1544 0.75 7.2 18

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) N_KU 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 21 P_C 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 21 Q_C 800KF9D 800 1 10 21 R_C 300KF9D 300 1 9 21 S_KU 300KF9D 300 1 9 21

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) K0001 K0024 A_KU 1 Ku-budgets.xls 57.2 20 23 46 49.68 -151.2 17.1 K0001 K0024 B_KU 1 Ku-budgets.xls 57.2 20 23 46 49.68 -150.2 17.1 K0001 K0024 C_KU 5 6950 Ku-budgets.xls 52.9 8.9 12 32 36.68 -157.2 25.6 K0001 K0024 D_KU 6 5000 Ku-budgets.xls 52.9 8.9 12 32 35.68 -157.2 25.6 K0001 K0024 E_KU 250 100 Ku-budgets.xls 46.6 -5 -3 16 19.48 -152.9 19.6 K0001 K0024 F_KU 20 1544 Ku-budgets.xls 46.6 8 11 26 29.48 -157.3 25.6 K0001 K0024 G_KU 1 Ku-budgets.xls 57.2 20 23 46 49.68 -150.9 25.6 C0001 C0024 H_C 1 C-budgets.xls 54.4 17.1 20.1 37 41.98 -158.9 21.8 C0001 C0024 I_C 5 C-budgets.xls 54.4 9.6 15 27 31.98 -161.9 25.2 C0001 C0024 J_C 1 C-budgets.xls 54.4 22 25 37 41.98 -159.4 33.2 C0001 C0024 K_C 1 C-budgets.xls 54.4 22 25 37 41.98 -159.6 33.2 C0001 C0024 L_C 250 100 C-budgets.xls 47.4 -3.4 2 7 11.98 -160 23 C0001 C0024 M_C 20 1544 C-budgets.xls 47.4 11 16 24 29.2 -157.2 23 K0001 K0024 N_KU 1 Ku-budgets.xls 6000 57.2 17 25 46 49.7 -139.3 19.6 C0001 C0024 P_C 1 C-budgets.xls 6000 49.8 17 25 36 41.98 -141 23 C1 C1 Q_C 1 TTC-budgets.xl 54.4 13 16 T1 T2 R_C 1 TTC-budgets.xl 14.3 18.3 -162.8 31 T3 T3 S_KU 1 TTC-budgets.xl 12.4 16.4 -164.7 38.3

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): 410-548-4300 E7169 Remote Control (TT C) Location(s): S14a: Street Address: Vernon Valley Spacecrafts 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

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: 2010-03-25 10:34:50
Document Modified: 2010-03-25 10:34:50
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