Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20050822-00165 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2005082200165_450884

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: DIRECTV 9S(K) 7/15/2006 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 11/1/2003 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 11/30/2005 2 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: 1/1/2006 6/30/2006 1000 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) 28.35 G 28.6 G R Fixed Satellite Service 29.25 G 29.5 G R Fixed Satellite Service 29.5 G 30.0 G R Fixed Satellite Service 18.3 G 18.8 G T Fixed Satellite Service 19.7 G 20.2 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: 101.125 W 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 (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) LABC S Area around Los Angeles, CA MWBC S Area around Minneapolis, MN TUSCAZ S Area around Tuscon, AZ BOISEID S Area around Boise, ID

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) UL1 R 47.6 46.3 0.08 27 Y LABC 3548 12.1 -105 31 1 UL2 R 48.4 47.3 0.08 27 Y BOISEID 4266 12.1 -105 31 1 DL1 T 50.1 49.5 0.08 27 N TUSCAZ 3.9 0.36 41.8 DL2 T 52.4 51.6 0.08 27 N MWBC 3.9 0.21 41.8

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) RB02 T C -101 RB02_C.gxt BB03 T C -101 BB03_C.gxt RB04 T C -101 RB04_C.gxt RB05 T C -101 RB05_C.gxt RB06 T C -101 RB06_C.gxt BB07 T C -101 BB07_C.gxt BB08 T C -101 BB08_C.gxt BB09 T C -101 BB09_C.gxt BB10 T C -101 BB10_C.gxt BB11 T C -101 BB11_C.gxt CB12 T C -101 CB12_C.gxt CB13 T C -101 CB13_C.gxt CB14 T C -101 CB14_C.gxt CB15 T C -101 CB15_C.gxt CB16 T C -101 CB16_C.gxt CB17 T C -101 CB17_C.gxt CB18 T C -101 CB18_C.gxt CB19 T C -101 CB19_C.gxt CB20 T C -101 CB20_C.gxt BB21 T C -101 BB21_C.gxt DL1 T C -101 D9S Ka DL Tucson_final.gxt DL2 T C -101 D9S Ka DL MWBC_final.gxt BB22 T C -101 BB22_C.gxt BB23 T C -101 BB23_C.gxt BB24 T C -101 BB24_C.gxt RB25 T C -101 RB25_C.gxt RB26 T C -101 RB26_C.GXT UL1 R C -101 D9S Ka UL LABC_final.gxt

UL2 R C -101 D9S Ka UL BOIS_final.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 ID Gain (dB) No. ID No. (T or C) RL001 250000 R 28475 L C BH001 107 RL001 UL1 TR002 DL1 RR001 250000 R 28475 R C BH002 107 RR001 UL1 TL002 DL2 RL002 250000 R 29375 L C BH003 107 RL002 UL1 TR001 DL1 RR002 250000 R 29375 R C BH004 107 RR002 UL1 TL001 DL2 RL003 500000 R 29750 L C BH005 107 RL003 UL2 TR003 DL1 RR003 500000 R 29750 R C BH006 107 RR003 UL2 TL003 DL2 TL002 250000 T 18675 L C TR002 250000 T 18675 R C TL003 500000 T 19950 L C TR003 500000 T 19950 R C CMD 1000 R 17795 R T TLM1 1000 T 12695.5 R T TLM2 1000 T 12696.5 R T TL001 250000 T 18425 L C TR001 250000 T 18425 R 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) BSS1 24M0G7W 24000 4 30320 0.758 6.8 20 BSS2 36M0G7W 36000 4 45.48 0.758 6.8 20 BSS3 54M0G7W 54000 4 68.22 0.758 6.8 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) CMD 1M00F9D 1000 1 10 28 TLM 1M00F9D 1000 1 10 28

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) BH001 BH004 BSS1 8 30000 58.5 19 19 50.8 50.8 -134 32.9 BH001 BH004 BSS2 6 40000 66.8 14.3 14.3 49.6 49.6 -136 41 BH001 BH004 BSS3 4 60000 66.8 15.2 15.2 47.8 47.8 -138 41 BH005 BH006 BSS1 16 30000 58.5 19 19 50.8 50.8 -134 32.9 BH005 BH006 BSS2 12 40000 66.8 14.3 14.3 49.6 49.6 -136 41 BH005 BH006 BSS3 8 60000 66.8 15.2 15.2 47.8 47.8 -138 41

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: 1600 Forbes Way S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Long Beach Los Angeles CA 90810 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 310-525-5590 Remote Control (TT C) Location(s): S14a: Street Address: 33E Telegraph Rd. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Fillmore Ventura CA 93015 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 805-524-4444

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 2364 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 3140 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5685 31.3 0.85 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 984 12.1 0.84 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 59.6 7.5 0.73 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): 7581 7581 7581 7581 Bus (Watts): (b): (g): (l): (q): 2845 1788 2845 1788 Total (Watts): (c): (h): (m): (r): 10696 9639 10696 9639 Solar Array (Watts): (d): (i): (n): (s): 12710 11442 11820 10641 Depth of Battery (e) (j) (o) (t) Discharge (%): 80 % 0 % 80 % 0 % 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: 2005-08-23 13:54:23
Document Modified: 2005-08-23 13:54:23
© 2025 FCC.report
This site is not affiliated with or endorsed by the FCC