Attachment Sched S Tech Report

This document pretains to SAT-MOD-20110929-00192 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2011092900192_919247

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-5 11/30/1998 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 16 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: 10/28/1998 864 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) 14000 M 14500 M R 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 11700 M 12200 M T 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: 80.9 W Availability of a slot in the central part of the US arc, in Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be cooperation with Argentine operator N/S Station-Keeping provided (Optional): d. Toward West: Degrees E/W 0.1 Degrees Tolerance: g. Westernmost: e. Toward East: 0.1 Degrees 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) KUL S CONUS and parts of Canada, Caribbean and Alaska KDL S CONUS and parts of Canada, Caribbean and Alaska

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) KRH R 34.32 25 0.15 0 30 Y 0 KUL 460 6.58 -100.3 21 1 KRV R 34.3 25 0.15 0 30 Y 90 KUL 465 7.69 -104.3 21 1 KTH T 32.94 25 0.15 0 30 Y 0 KDL 2 34.75 48.35 KTV T 33.64 25 0.15 0 30 Y 90 KDL 2 34.75 49.05

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) KRH R C -80.9 XP7G2T_HPOL.gxt KRV R C -80.9 XP8G2T_VPOL.gxt KTH T C -80.9 XP8EIRP_HPOL.gxt KTV T C -80.9 XP7EIRP_VPOL.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) KR001 54000 R 14030 H C K0001 127.8 KR001 KRH KT001 KTV KR002 54000 R 14043 V C K0002 131.8 KR002 KRV KT002 KTH KR003 54000 R 14091 H C K0003 127.8 KR003 KRH KT003 KTV KR004 54000 R 14104 V C K0004 131.8 KR004 KRV KT004 KTH KR005 54000 R 14152 H C K0005 127.8 KR005 KRH KT005 KTV KR006 54000 R 14165 V C K0006 131.8 KR006 KRV KT006 KTH KR007 54000 R 14213 H C K0007 127.8 KR007 KRH KT007 KTV KR008 54000 R 14226 V C K0008 131.8 KR008 KRV KT008 KTH KR009 54000 R 14274 H C K0009 127.8 KR009 KRH KT009 KTV KR010 54000 R 14287 V C K0010 131.8 KR010 KRV KT010 KTH KR011 54000 R 14335 H C K0011 127.8 KR011 KRH KT011 KTV KR012 54000 R 14348 V C K0012 131.8 KR012 KRV KT012 KTH KR013 54000 R 14396 H C K0013 127.8 KR013 KRH KT013 KTV KR014 54000 R 14409 V C K0014 131.8 KR014 KRV KT014 KTH KR015 54000 R 14457 H C K0015 127.8 KR015 KRH KT015 KTV KR016 54000 R 14470 V C K0016 131.8 KR016 KRV KT016 KTH KT001 54000 T 11730 V C C1 TC KRV KT002 54000 T 11743 H C T1 TM1 KTH KT003 54000 T 11791 V C T2 TM2 KTH KT004 54000 T 11804 H C KT005 54000 T 11852 V C KT006 54000 T 11865 H C KT007 54000 T 11913 V C KT008 54000 T 11926 H C KT009 54000 T 11974 V C KT010 54000 T 11987 H C KT011 54000 T 12035 V C KT012 54000 T 12048 H C KT013 54000 T 12096 V C KT014 54000 T 12109 H C

KT015 54000 T 12157 V C KT016 54000 T 12170 H C TC 1000 R 14001 V T TM1 500 T 11701 H T TM2 500 T 11702 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) D1 36M0G7W 36000 4 40000 0.69 6.8 19 D2 27M0G7W 27000 4 32000 0.69 6.8 19 D3 54M0G7W 54000 4 60000 0.69 6.8 19 D4 5M00G1W 5000 4 6000 0.69 6.8 19 D5 100KG1W 100 4 56 0.69 6.8 19 D6 1M60G1W 1600 4 1544 0.69 6.8 19 D7 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) A1 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 20 A_TC 800KF9D 800 10 20 A_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) K0001 K0016 D1 1 AMC5 link budg 57.3 20 25 44 49 20.9 K0001 K0016 D2 1 AMC5 link budg 57.3 20 25 44 49 20.9 K0001 K0016 D3 1 AMC5 link budg 57.3 20 25 45 49 20.9 K0001 K0016 D4 6 5000 AMC5 link budg 53 8.9 14 32 35 26.9 K0001 K0016 D5 250 100 AMC5 link budg 46.7 -2 3 16 20 20.9 K0001 K0016 D6 20 1544 AMC5 link budg 46.7 8 13 25 30 26.9 K0001 K0016 D7 1 AMC5 link budg 57.3 20 25 44 49 26.9 K0001 K0016 A1 1 AMC5 link budg 2000 57.3 19 22 44 49 20.9 C1 C1 A_TC 1 TTandC Tables 60.2 10 15 T1 T2 A_TM 1 TTandC Tables 15 29 33.2

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 E900448 Remote Control (TT C) Location(s): S14a: Street Address: Brewster Teleport S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Brewster WA 98812 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 509-689-6000 E060416

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 769.3 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1771.9 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 1724.6 22.2 0.94 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 267.3 2.1 0.89 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 28.3 1.6 0.84 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): 1865 1865 1865 1865 Bus (Watts): (b): (g): (l): (q): 677 458 737 476 Total (Watts): (c): (h): (m): (r): 2542 2323 2602 2341 Solar Array (Watts): (d): (i): (n): (s): 3462 3122 3048 2784 Depth of Battery (e) (j) (o) (t) Discharge (%): % % 68 % 68 % 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: 2011-09-30 08:34:00
Document Modified: 2011-09-30 08:34:00
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