Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20050325-00075 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2005032500075_425280

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: SATCOM SN-4 6/18/1991 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 24 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: 1296 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 14.00 G 14.50 G R Fixed Satellite Service 11.70 G 12.20 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: 172 E 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 0.1 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 (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) POR-C-UL E Pacific Ocean Region, G/T contours, Service area: -9 dB/K contour POR-C-DL E Pacific Ocean Region, EIRP contours, Service area: 28 dBW contour POR-KU-UL E Pacific Ocean Region, G/T contours, Service area: -6 dB/K contour POR-KU-DL E Pacific Ocean Region, EIRP contours, Service area: 33 dBW contour N/A N/A

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) CRH R 30.2 15.2 0.15 0 30 N 0 POR-C-UL 840 0.96 -83 3 3 CRV R 27.8 22.8 0.15 0 30 N 90 POR-C-UL 760 -1.1 -83 3 3 CTH T 29.5 24.5 0.15 0 30 N 0 POR-C-DL 1 6.8 37.8 CTV T 28.2 13.2 0.15 0 30 N 90 POR-C-DL 1 6.8 36.5 KRV R 31.6 16.6 0.15 0 30 N 90 POR-KU- 891 2.1 -87 6 6 KTH T 33.3 18.3 0.15 0 30 N 0 POR-KU- 1 23.9 47.1

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 172 CRH.gxt CRV R C 172 CRV.gxt CTH T C 172 CTH.gxt -156 -156 -156 -156 -156 CTV T C 172 CTV.gxt -157.8 -157.8 -157.8 -157.8 -157.8 KRV R C 172 KRV.gxt KTH T C 172 KTH.gxt -151 -151 -151 -151 -151

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) C1R 36000 R 5945 H C C1 106 C1R CRH C1T CTV C2R 36000 R 5985 H C C2 106 C2R CRH C2T CTV C3R 36000 R 6025 H C C3 106 C3R CRH C3T CTV C4R 36000 R 6065 H C C4 106 C4R CRH C4T CTV C5R 36000 R 6105 H C C5 106 C5R CRH C5T CTV C6R 36000 R 6145 H C C6 106 C6R CRH C6T CTV C7R 36000 R 5965 V C C7 108 C7R CRV C7T CTH C8R 36000 R 6005 V C C8 108 C8R CRV C8T CTH C9R 36000 R 6045 V C C9 108 C9R CRV C9T CTH C10R 36000 R 6085 V C C10 108 C10R CRV C10T CTH C11R 36000 R 6125 V C C11 108 C11R CRV C11T CTH C12R 36000 R 6165 V C C12 108 C12R CRV C12T CTH C13R 72000 R 6205 H C C13 106 C13R CRH C13T CTV C14R 72000 R 6285 H C C14 106 C14R CRH C14T CTV C15R 72000 R 6365 H C C15 106 C15R CRH C15T CTV C16R 72000 R 6225 V C C16 108 C16R CRV C16T CTH C17R 72000 R 6305 V C C17 108 C17R CRV C17T CTH C18R 72000 R 6385 V C C18 108 C18R CRV C18T CTH K1R 72000 R 14040 V C K1 114 K1R KRV K1T KTH K2R 72000 R 14120 V C K2 114 K2R KRV K2T KTH K3R 72000 R 14200 V C K3 114 K3R KRV K3T KTH K4R 72000 R 14280 V C K4 114 K4R KRV K4T KTH K5R 72000 R 14360 V C K5 114 K5R KRV K5T KTH K6R 72000 R 14440 V C K6 114 K6R KRV K6T KTH C1T 36000 T 3720 V C C2T 36000 T 3760 V C C3T 36000 T 3800 V C C4T 36000 T 3840 V C C5T 36000 T 3880 V C C6T 36000 T 3920 V C

C7T 36000 T 3740 H C C8T 36000 T 3780 H C C9T 36000 T 3820 H C C10T 36000 T 3860 H C C11T 36000 T 3900 H C C12T 36000 T 3940 H C C13T 72000 T 3980 V C C14T 72000 T 4060 V C C15T 72000 T 4140 V C C16T 72000 T 4000 H C C17T 72000 T 4080 H C C18T 72000 T 4160 H C K1T 72000 T 11740 H C K2T 72000 T 11820 H C K3T 72000 T 11900 H C K4T 72000 T 11980 H C K5T 72000 T 12060 H C K6T 72000 T 12140 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) C1 C18 A 1 C_band_link_b 53.7 26 30 31 37 -165.1 23 C1 C18 B 5 6950 C_band_link_b 47.3 13 17 20 26 -168.9 23 C1 C18 C 1 C_band_link_b 53.7 26 30 31 37 -165.1 23 C1 C18 D 1 C_band_link_b 53.7 26 30 31 37 -165.1 29 C1 C18 E 360 100 C_band_link_b 47.3 6 10 1.4 7.4 -169.1 23 C1 C18 F 26 1350 C_band_link_b 47.3 13 17 12.9 18.9 -169 23 C1 C18 G 1 C_band_link_b 6000 53.7 22.5 26.5 31 37 -157.3 23 K1 K6 A 1 Ku_band_link_ 57.2 26 30 37.5 47.5 -154.6 25.6 K1 K6 B 5 6950 Ku_band_link_ 52.8 13 17 26.5 36.5 -158.4 25.6 K1 K6 C 1 Ku_band_link_ 57.2 26 30 37.5 47.5 -154.6 25.6 K1 K6 D 1 Ku_band_link_ 57.2 26 30 37.5 47.5 -154.6 35.6 K1 K6 E 360 100 Ku_band_link_ 46.6 6 10 7.9 17.9 -158.6 25.6 K1 K6 F 26 1350 Ku_band_link_ 52.8 13 17 19.4 29.4 -158.5 25.6 K1 K6 G 1 Ku_band_link_ 6000 59.1 22.5 26.5 38 43 -151.3 25.6

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 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): 4105494300 E7169

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 572 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 623 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 692 11.7 0.5 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 120 1.6 0.88 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 11.7 3 0.44 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): 1054 1054 1054 1054 Bus (Watts): (b): (g): (l): (q): 152 126 142 116 Total (Watts): (c): (h): (m): (r): 1206 1180 1196 1170 Solar Array (Watts): (d): (i): (n): (s): 1794 1631 1433 1303 Depth of Battery (e) (j) (o) (t) Discharge (%): 68 % 68 % 67 % 67 % 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? X 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? 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: 2005-03-30 08:38:49
Document Modified: 2005-03-30 08:38:49
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