Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20060119-00004 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2006011900004_477060

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 13 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: 3 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: 82 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) 17.3 G 17.8 G R Fixed Satellite Service 12.2 G 12.7 G T Broadcasting Satellite Service - Video 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: 109.8 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) CONUS1 S CONUS LACR1 S Los Angeles, CA+Castle Rock, CO AKHI S Alaska+Hawaii

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) DL_1 T 36.4 30.4 0.2 30 N CONUS1 2.7 600 61.5 UL1 R 35 31 0.2 30 N LACR1 900 5.5 -93.5 20 1 DL2 T 36 30 0.2 30 N AKHI 3 56.2 50.5

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) DL_1 T C -101 DPTX_co.gxt DL2 T C -101 AHTX_co.gxt UL1 R C -101 DPRX_co.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) R028 24000 R 17717.66 L C T0001 133.6 R028 UL1 T028 DL_1 R030 24000 R 17746.82 L C T0002 133.6 R030 UL1 T030 DL_1 R032 24000 R 17775.98 L C T0003 133.6 R032 UL1 T032 DL_1 RWB1A 36000 R 17724 L C T0004 133.6 RWB1A UL1 TWB1A DL_1 RWB1B 36000 R 17770 L C T0005 133.6 RWB1B UL1 TWB1B DL_1 RWB2A 82000 R 17746.82 L C T0006 133.6 RWB2A UL1 TWB2A DL_1 T028 24000 T 12617.66 L C T0007 133.6 R028 UL1 T028 DL2 T030 24000 T 12646.82 L C T0008 133.6 R030 UL1 T030 DL2 T032 24000 T 12675.98 L C T0009 133.6 R032 UL1 T032 DL2 TWB1A 36000 T 12624 L C T0010 133.6 RWB1A UL1 TWB1A DL2 TWB1B 36000 T 12670 L C T0011 133.6 RWB1B UL1 TWB1B DL2 TWB2A 82000 T 12646.82 L C T0012 133.6 RWB2A UL1 TWB2A DL2 CMD1 1000 R 17305 L T TLMA TLM1 DL_1 CMD2 1000 R 17307 L T TLMB TLM2 DL_1 TLM1 1000 T 12203 L T CMDA CMD1 UL1 TLM2 1000 T 12204 L T CMDB CMD2 UL1

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) DTH 24M0G7W 24000 4 40000 0.48 7.6 28 DTH2 36M0G7W 36000 4 60000 0.48 7.6 28 DTH3 82M0G7W 82000 4 136700 0.48 7.6 28

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) TLM 1M00F9D 1000 1 7.6 28 CMD 1M00F9D 1000 1 7.6 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) T0001 T0006 DTH 1 64.2 12.8 21.8 52 58 4.9 T0001 T0006 DTH2 1 64.2 14.6 23.6 53.8 59.8 4.9 T0001 T0006 DTH3 1 64.2 18.1 27.1 55.5 61.5 4.9 T0007 T0012 DTH 1 64.2 12.8 21.8 41 47 13 T0007 T0012 DTH2 1 64.2 14.6 23.6 42.8 48.8 13 T0007 T0012 DTH3 1 64.2 18.1 27.1 44.5 50.5 13 TLMA TLMB TLM 1 12 18.3 40 CMDA CMDB CMD 1 64.2 -3.6 48.4

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): No

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 1480 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2230 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3710 31.3 0.8845 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 2060 8.7 0.9115 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 60.6 6.2 0.8062 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): 5958 5958 5800 5800 Bus (Watts): (b): (g): (l): (q): 1864 955 1900 900 Total (Watts): (c): (h): (m): (r): 7833 6913 7700 6700 Solar Array (Watts): (d): (i): (n): (s): 9340 8379 8400 7659 Depth of Battery (e) (j) (o) (t) Discharge (%): 74 % 0 % 72 % 0 % 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? 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: 2006-01-20 11:25:20
Document Modified: 2006-01-20 11:25:20
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