Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20060811-00087 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2006081100087_518975

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 4R N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 48 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: 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) 5925 M 6425 M R Fixed Satellite Service 3700 M 4200 M T Fixed Satellite Service 14.0 G 14.5 G R Fixed Satellite Service 11.7 G 12.2 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: 76.85 W PROVIDE SERVICE CONTINENTAL UNITED Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be STATES, HAWAII, ALASKA, SOUTHERN CANADA, N/S Station-Keeping provided (Optional): MEXICO AND CARRIBEAN ISLANDS 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, ALASKA, SOUTHERN CANADA, MEXICO AND THE CARRIBEAN 2 S NORTH AMERICA 3 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) CHU R 29.5 25.5 0.2 0.7 30 Y 01 0 -96 16 2 CVU R 29.5 25.5 0.2 0.7 30 Y 90 1 0 -96 16 2 CHD T 29.6 25.6 0.2 0.7 30 Y 0 1 42.1 CVD T 29.6 25.6 0.2 0.7 30 Y 90 1 42.1 KHU R 33.3 27.3 0.2 0.7 30 Y 0 1 4.4 -98.4 16 2 KVU R 33.3 27.3 0.2 0.7 30 Y 90 1 4.4 -98.4 16 2 KHD T 30.9 26.9 0.2 0.7 30 Y 0 1 47.9 KVD T 30.9 26.9 0.2 0.7 30 Y 90 1 47.9 CMD R 29.5 19.5 0.2 0.7 Y 90 1 -9.6 -114.4 CMD R 5.1 3.1 0.2 0.7 N 3 -29 -96.7 CMD R -2.3 -5.3 0.2 0.7 N 03 -34.7 -90.1 TLM T 29.9 19.9 0.2 0.7 Y 01 18.6 TLM T 5.8 3.8 0.2 0.7 N 3 12.1 TLM T -0.4 -3.4 0.2 0.7 N 90 3 8.5 UPC T 22.8 18.8 0.2 0.7 Y 02 15.8 UPC T 22.8 18.8 0.2 0.7 Y 90 2 15.8

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) CHU R C 76.85 CHUP.gxt CVU R C 76.85 CVUP.gxt CHD T C 76.85 CHDN.gxt -152 -151.1 -150.9 -150.8 -150.7 CVD T C 76.85 CVDN.gxt -152 -151.1 -150.9 -150.8 -150.7 KHU R C 76.85 KHUP.gxt KVU R C 76.85 KVUP.gxt KHD T C 76.85 KHDN.gxt KVD T C 76.85 KVDN.gxt CMD R C 76.85 CMDC.gxt CMD R C 76.85 CMDP.pdf CMD R C 76.85 CMDB.pdf TLM T C 76.85 TLMC.gxt TLM T C 76.85 TLMP.pdf TLM T C 76.85 TLMB.pdf UPC T C 76.85 UPCH.pdf UPC T C 76.85 UPCV.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) CU1 36000 R 5945 V C 1C 116.3 CU1 CVUP CD1 CHDN CU3 36000 R 5985 V C 3C 116.3 CU3 CVUP CD3 CHDN CU5 36000 R 6025 V C 5C 116.3 CU5 CVUP CD5 CHDN CU7 36000 R 6065 V C 7C 116.3 CU7 CVUP CD7 CHDN CU9 36000 R 6105 V C 9C 116.3 CU9 CVUP CD9 CHDN CU11 36000 R 6145 V C 11C 116.3 CU11 CVUP CD11 CHDN CU13 36000 R 6185 V C 13C 116.3 CU13 CVUP CD13 CHDN CU15 36000 R 6225 V C 15C 116.3 CU15 CVUP CD15 CHDN CU17 36000 R 6265 V C 17C 116.3 CU17 CVUP CD17 CHDN CU19 36000 R 6305 V C 19C 116.3 CU19 CVUP CD19 CHDN CU21 36000 R 6345 V C 21C 116.3 CU21 CVUP CD21 CHDN CU23 36000 R 6385 V C 23C 116.3 CU23 CVUP CD23 CHDN CU2 36000 R 5965 H C 2C 116.3 CU2 CHUP CD2 CVDN CU4 36000 R 6005 H C 4C 116.3 CU4 CHUP CD4 CVDN CU6 36000 R 6045 H C 6C 116.3 CU6 CHUP CD6 CVDN CU8 36000 R 6085 H C 8C 116.3 CU8 CHUP CD8 CVDN CU10 36000 R 6125 H C 10C 116.3 CU10 CHUP CD10 CVDN CU12 36000 R 6165 H C 12C 116.3 CU12 CHUP CD12 CVDN CU14 36000 R 6205 H C 14C 116.3 CU14 CHUP CD14 CVDN CU16 36000 R 6245 H C 16C 116.3 CU16 CHUP CD16 CVDN CU18 36000 R 6285 H C 18C 116.3 CU18 CHUP CD18 CVDN CU20 36000 R 6325 H C 20C 116.3 CU20 CHUP CD20 CVDN CU22 36000 R 6365 H C 22C 116.3 CU22 CHUP CD22 CVDN CU24 36000 R 6405 H C 24C 116.3 CU24 CHUP CD24 CVDN CD1 36000 T 3720 H C 1K 126.6 KU1 KVUP KD1 KHDN CD3 36000 T 3760 H C 3K 126.6 KU3 KVUP KD3 KHDN CD5 36000 T 3800 H C 5K 126.6 KU5 KVUP KD5 KHDN CD7 36000 T 3840 H C 7K 126.6 KU7 KVUP KD7 KHDN CD9 36000 T 3880 H C 9K 126.6 KU9 KVUP KD9 KHDN CD11 36000 T 3920 H C 11K 126.6 KU11 KVUP KD11 KHDN

CD13 36000 T 3960 H C 13K 126.6 KU13 KVUP KD13 KHDN CD15 36000 T 4000 H C 15K 126.6 KU15 KVUP KD15 KHDN CD17 36000 T 4040 H C 17K 126.6 KU17 KVUP KD17 KHDN CD19 36000 T 4080 H C 19K 126.6 KU19 KVUP KD19 KHDN CD21 36000 T 4120 H C 21K 126.6 KU21 KVUP KD21 KHDN CD23 36000 T 4160 H C 23K 126.6 KU23 KVUP KD23 KHDN KU1 36000 R 14020 V C 2K 126.6 KU2 KHUP KD2 KVDN KU3 36000 R 14060 V C 4K 126.6 KU4 KHUP KD4 KVDN KU5 36000 R 14100 V C 6K 126.6 KU6 KHUP KD6 KVDN KU7 36000 R 14140 V C 8K 126.6 KU8 KHUP KD8 KVDN KU9 36000 R 14180 V C 10K 126.6 KU10 KHUP KD10 KVDN KU11 36000 R 14220 V C 12K 126.6 KU12 KHUP KD12 KVDN KU13 36000 R 14260 V C 14K 126.6 KU14 KHUP KD14 KVDN KU15 36000 R 14300 V C 16K 126.6 KU16 KHUP KD16 KVDN KU17 36000 R 14340 V C 18K 126.6 KU18 KHUP KD18 KVDN KU19 36000 R 14380 V C 20K 126.6 KU20 KHUP KD20 KVDN KU21 36000 R 14420 V C 22K 126.6 KU22 KHUP KD22 KVDN KU23 36000 R 14460 V C 24K 126.6 KU24 KHUP KD24 KVDN KU2 36000 R 14040 H C KU4 36000 R 14080 H C KU6 36000 R 14120 H C KU8 36000 R 14160 H C KU10 36000 R 14200 H C KU12 36000 R 14240 H C KU14 36000 R 14280 H C KU16 36000 R 14320 H C KU18 36000 R 14360 H C KU20 36000 R 14400 H C KU22 36000 R 14440 H C KU24 36000 R 14480 H C KD1 36000 T 11720 H C KD3 36000 T 11760 H C KD5 36000 T 11800 H C KD7 36000 T 11840 H C KD9 36000 T 11880 H C KD11 36000 T 11920 H C KD13 36000 T 11960 H C KD15 36000 T 12000 H C KD17 36000 T 12040 H C

KD19 36000 T 12080 H C KD21 36000 T 12120 H C KD23 36000 T 12160 H C KD2 36000 T 11740 V C KD4 36000 T 11780 V C KD6 36000 T 11820 V C KD8 36000 T 11860 V C KD10 36000 T 11900 V C KD12 36000 T 11940 V C KD14 36000 T 11980 V C KD16 36000 T 12020 V C KD18 36000 T 12060 V C KD20 36000 T 12100 V C KD22 36000 T 12140 V C KD24 36000 T 12180 V C CMD1 1000 R 6422.25 V T CMD2 1000 R 6422.25 H T CMD3 1000 R 5926.75 R T TLM1 500 T 4198.125 H T TLM2 500 T 4199.625 H T CD2 36000 T 3740 V C CD4 36000 T 3780 V C CD6 36000 T 3820 V C CD8 36000 T 3860 V C CD10 36000 T 3900 V C CD12 36000 T 3940 V C CD14 36000 T 3980 V C CD16 36000 T 4020 V C CD18 36000 T 4060 V C CD20 36000 T 4100 V C CD22 36000 T 4140 V C CD24 36000 T 4180 V C TLM3 500 T 4198.125 V T TLM4 500 T 4199.625 V T TLM5 500 T 4198.125 R T TLM6 500 T 4199.625 R T ULPC1 25 T 11701 V C ULPC2 25 T 12195 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) D1 30M1G7W 30133 4 36863 0.75 6.1 13.6 D2 4M15G7W 4154 4 6000 0.75 6.7 14.2 D3 1M21G7W 1212.8 4 1544 0.75 5.7 13.1 D4 75K4G7W 75.4 4 64 0.5 3 10.4 D5 30M1G7W 30133 4 36863 0.75 6.1 21.8 D6 4M15G7W 4154 4 6000 0.75 6.7 19.6 D7 1M21G7W 1212.8 4 1544 0.75 5.7 19.1 D8 75K4G7W 75.4 4 64 0.5 3 17.1 D9 1M23G7W 1229 2 512 0.5 3.4 17 D10 307KG7W 307 2 128 0.5 3.4 15

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 2.56 10 15.2 A2 36M0F3F 36000 TV/FM 1 NTSC 12.8 2.56 10 23.9

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) 1C 24C A1 1 C-BAND LINK 4000 51 19.9 23.9 38.1 42.1 -150 28.4 1C 24C D1 1 C-BAND LINK 51 19.9 23.9 38.1 42.1 -158.7 21 1C 24C D2 3 C-BAND LINK 51 13.4 17.4 29.1 33.1 -159.1 21 1C 24C D3 15 C-BAND LINK 51 6.9 10.9 22.6 26.6 -160.3 21 1C 24C D4 360 C-BAND LINK 51 -7.8 -3.8 7.9 11.9 -162.9 21 1K 24K A2 1 KU-BAND LINK 4000 58.1 11.7 17.7 39 43 -149.1 33.1 1K 24K D5 1 KU-BAND LINK 58.1 13.8 19.8 40.8 44.8 -156.1 25 1K 24K D6 4 KU-BAND LINK 58.1 -2.4 3.6 32.2 36.2 -156.1 26.7 1K 24K D7 16 KU-BAND LINK 58.1 -7.8 -1.8 26.9 30.9 -156 25 1K 24K D8 318 KU-BAND LINK 58.1 -20 -14.6 14.1 18.1 -156.8 22.3 1K 24K D9 20 KU-BAND LINK 58.1 -8.6 -2.6 26.1 30.1 -156.9 22.3 1K 24K D10 90 KU-BAND LINK 46.4 -8.1 -2.1 14.9 18.9 -162.1 34.6

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

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: S16. SPACECRAFT ELECTRICAL CHARACTERISTICS: S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: 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 # 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? 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: 2006-08-14 10:48:11
Document Modified: 2006-08-14 10:48:11
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC