Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20040909-00168 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2004090900168_395567

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 11 3/30/2007 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 9/1/2004 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 11/30/2006 24 0 MHz d. Estimated Launch Date: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply: 12/20/2006 960 MHz GSO NGSO 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) 18.3 G 18.8 G T Direct to Home in the Fixed Fixed Satellite Service 28.35 G 28.6 G R Fixed Satellite Service 29.25 G 29.5 G R Fixed Satellite Service 18.3 G 18.8 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: 99.05 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 Degrees E/W 0.05 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) CONUS+ S CONUS + Alaska LABC S Uplink beam centered on Los Angeles, CA CRBC S Uplink beam centered on Castle Rock, CO SPOT1 S Downlink beam centered on New York, NY SPOT2 S Downlink beam centered on Minneapolis, MN SPOT3 S Downlink beam centered on Colorado Springs, CO CMD S Colorado Springs, CO

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 Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) Pt. (dBW/m2) UL1 R 47.5 46.5 0.1 27 N LABC 891 18 -105 19 1 UL2 R 46.5 46.5 0.1 27 N CRBC 891 18 -105 19 1 DL1 T 36.1 30.1 0.1 27 N CONUS+ 2 260 58.3 A1B1 T 48.1 45.1 0.1 27 N SPOT1 2.9 26.9 59.5 A1B7 T 48.1 45.1 0.1 27 N SPOT2 2.9 26.9 59.5 A1B9 T 48.1 45.1 0.1 27 N SPOT3 2.9 26.9 59.5 CMD R 38.5 37.5 0.1 27 N CMD 17783 -4

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) UL1 R C -99 UL-LA (99.0W)_R1.gxt UL2 R C -99 UL-CR (99.0W)_R1.gxt DL1 T C -99 CONUS(99.0W)_R2.gxt -126 -126 -126 -128 -127 A1B1 T C -99 A1B1(99.0W)_R1.gxt -126 -126 -126 -128 -127 A1B7 T C -99 A1B7(99.0W)_R1.gxt -126 -126 -126 -128 -127 A1B9 T C -99 A1B9(99.0W).gxt -126 -126 -126 -128 -127 CMD R C -99 CMD_Beam 99W.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) (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band Channel Assigned T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID No. Bandwidth Mode (MHz) (H, V, L, R) Channel ID Gain (dB) No. ID No. (kHz) (T or C) T0013 36000 T 18564 R C NAT1 121 R0001 UL1 T0001 DL1 T0015 36000 T 18604 R C NAT2 121 R0002 UL1 T0002 DL1 T0013 36000 T 18564 R C NAT3 121 R0003 UL1 T0003 DL1 T0015 36000 T 18604 R C NAT4 121 R0004 UL1 T0004 DL1 T0017 36000 T 18648 R C NAT5 121 R0005 UL1 T0005 DL1 T0019 36000 T 18692 R C NAT6 121 R0006 UL1 T0006 DL1 T0021 36000 T 18732 R C NAT7 121 R0007 UL1 T0007 DL1 T0023 36000 T 18776 R C NAT8 121 R0008 UL1 T0008 DL1 T0002 36000 T 18324 L C NAT9 121 R0009 UL1 T0009 DL1 T0004 36000 T 18364 L C NAT10 121 R0010 UL1 T0010 DL1 T0006 36000 T 18404 L C NAT11 121 R0011 UL1 T0011 DL1 T0008 36000 T 18444 L C NAT12 121 R0012 UL1 T0012 DL1 T0010 36000 T 18484 L C NAT13 121 R0013 UL1 T0013 DL1 T0012 36000 T 18524 L C NAT14 121 R0014 UL1 T0014 DL1 T0014 36000 T 18564 L C LIL1 113 R016L T0016 A1B1 T0016 36000 T 18604 L C LIL2 113 R019L T0019 A1B1 T0018 36000 T 18648 L C LIL3 113 R020L T0020 A1B1 T0020 36000 T 18692 L C LIL4 113 R016U T0016 A1B7 T0022 36000 T 18732 L C LIL5 113 R019U T0019 A1B7 T0024 36000 T 18776 L C LIL6 113 R020U T0020 A1B7 CMD1 1300 R 29493 L T LIL7 113 R016U T0016 A1B9 CMD1B 1300 R 29251 L T LIL8 113 R019U T0019 A1B9 CMD2 1300 R 29495 L T CMD1 CMD1 CMD CMD2B 1300 R 29253 L T CMD1B CMD1B CMD CMD3 1300 R 29497 L T CMD2 CMD2 CMD CMD3B 1300 R 29255 L T CMD2B CMD2B CMD TLM1 106 T 18300.25 L T CMD3 CMD3 CMD TLM1B 106 T 18300.75 L T CMD3B CMD3B CMD TLM2 106 T 18301.25 L T TLM1 TLM1 DL1 TLM2B 106 T 18301.75 L T TLM1B TLM1B DL1

TLM3 106 T 18302.25 L T TLM2 TLM2 DL1 TLM3B 106 T 18302.75 L T TLM2B TLM2B DL1 R0001 36000 R 28375 R C TLM3 TLM3 DL1 R0003 36000 R 28415 R C TLM3B TLM3B DL1 R0005 36000 R 28455 R C R0007 36000 R 28495 R C R0009 36000 R 28535 R C R0011 36000 R 28575 R C R0002 36000 R 28375 L C R0004 36000 R 28415 L C R0006 36000 R 28455 L C R0008 36000 R 28495 L C R0010 36000 R 28535 L C R0012 36000 R 28575 L C R0013 36000 R 29269 R C R0014 36000 R 29269 L C R0015 36000 R 29309 R C R0016 36000 R 29309 L C R0017 36000 R 29353 R C R0018 36000 R 29353 L C R0019 36000 R 29397 R C R0020 36000 R 29397 L C R0021 36000 R 29437 R C R0022 36000 R 29437 L C R0023 36000 R 29481 R C R0024 36000 R 29481 L C R015L 36000 R 28389 R C R016L 36000 R 28389 L C R017L 36000 R 28433 R C R018L 36000 R 28433 L C R019L 36000 R 28477 R C R020L 36000 R 28477 L C R021L 36000 R 28517 R C R022L 36000 R 28517 L C R023L 36000 R 28561 R C R024L 36000 R 28561 L C R015U 36000 R 29285 R C R016U 36000 R 29285 L C R017U 36000 R 29329 R C

R018U 36000 R 29329 L C R019U 36000 R 29373 R C R020U 36000 R 29373 L C R021U 36000 R 29413 R C R022U 36000 R 29413 L C R023U 36000 R 29457 R C R024U 36000 R 29457 L C T0001 36000 T 18324 R C T0003 36000 T 18364 R C T0005 36000 T 18404 R C T0007 36000 T 18444 R C T0009 36000 T 18484 R C T0011 36000 T 18524 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) M2 36M0G7W 36000 4 35640 0.594 4.4 17 M3 36M0G7W 36000 4 39675 0.6613 5.2 14.8

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. Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective Companded Baseband Baseband Modulation ID (kHz) PAL, etc. (dB) Modulation and Noise (dB) (dB) Talker Level Freq. (MHz) Freq. (MHz) Index Index Weighting (dB) (dBm0) C1 1M30F9D 1300 1 15 40.4 T1 106KG9D 106 1 14 11.7

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) NAT1 NAT14 M3 1 64.3 7.6 12.6 52.2 58.2 -119.3 18.4 LIL1 LIL8 M2 1 64.3 7.6 12.6 56.5 59.5 -118 18.4 CMD1 CMD3B C1 1 66 21.6 21.6 TLM1 TLM3B T1 1 10 10 -152 31

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

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 3556 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2440 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 5996 47.9 0.6 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 266 8.2 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 77 7.3 0.51 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): 14330 14330 14330 14330 Bus (Watts): (b): (g): (l): (q): 1800 700 1800 700 Total (Watts): (c): (h): (m): (r): 16130 15030 16130 15030 Solar Array (Watts): (d): (i): (n): (s): 20050 17900 16900 15700 Depth of Battery (e) (j) (o) (t) Discharge (%): 79.5 % 0 % 79.5 % 0 % 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: 2004-09-09 16:13:38
Document Modified: 2004-09-09 16:13:38
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC