Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20060908-00100 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2006090800100_526461

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 BSS-103W 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: 24 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: 864 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) 24.75 G 25.25 G R Feeder Link for Broadcasting Satellite Service in FSS 17.3 G 17.8 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: 103 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) AMER S CONUS+AK+HI+PR MEX S Mexico LATAMER S South America

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 37 33 0.2 30 N AMER 900 7.4 -94 20 1 DL1 T 35.5 25.5 0.2 30 N AMER 1.5 400 60 DL2 T 36.4 30.4 0.2 30 N MEX 2.4 400 60 DL3 T 35.3 29.3 0.2 30 N LATAMER 1.3 400 60

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) DL1 T C -103 US-PR Transmit.gxt UL1 R C -103 US Receive.gxt DL2 T C -103 Mexico Transmit.gxt DL3 T C -103 S.America Transmit.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) T01 36000 T 17330 R C AM01 130 R01 UL1 T01 DL1 T02 36000 T 17330 L C AM02 130 R02 UL1 T02 DL1 T03 36000 T 17370 R C AM03 130 R03 UL1 T03 DL1 T04 36000 T 17370 L C AM04 130 R04 UL1 T04 DL1 T05 36000 T 17410 R C AM05 130 R05 UL1 T05 DL1 T06 36000 T 17410 L C AM06 130 R06 UL1 T06 DL1 T07 36000 T 17450 R C AM07 130 R07 UL1 T07 DL1 T08 36000 T 17450 L C AM08 130 R08 UL1 T08 DL1 T09 36000 T 17490 R C AM09 130 R09 UL1 T09 DL1 T10 36000 T 17490 L C AM10 130 R10 UL1 T10 DL1 T11 36000 T 17530 R C AM11 130 R11 UL1 T11 DL1 T12 36000 T 17530 L C AM12 130 R12 UL1 T12 DL1 T13 36000 T 17570 R C AM13 130 R13 UL1 T13 DL1 T14 36000 T 17570 L C AM14 130 R14 UL1 T14 DL1 T15 36000 T 17610 R C AM15 130 R15 UL1 T15 DL1 T16 36000 T 17610 L C AM16 130 R16 UL1 T16 DL1 T17 36000 T 17650 R C AM17 130 R17 UL1 T17 DL1 T18 36000 T 17650 L C AM18 130 R18 UL1 T18 DL1 T19 36000 T 17690 R C AM19 130 R19A UL1 T19A DL1 T20 36000 T 17690 L C AM20 130 R20A UL1 T20A DL1 T21 36000 T 17730 R C MX01 130 R01 UL1 T01 DL2 T22 36000 T 17730 L C MX02 130 R02 UL1 T02 DL2 T23 36000 T 17770 R C MX03 130 R03 UL1 T03 DL2 T24 36000 T 17770 L C MX04 130 R04 UL1 T04 DL2 T19A 24000 T 17684 R C MX05 130 R05 UL1 T05 DL2 T20A 24000 T 17684 L C MX06 130 R06 UL1 T06 DL2 R01 36000 R 24780 R C MX07 130 R07 UL1 T07 DL2 R02 36000 R 24780 L C MX08 130 R08 UL1 T08 DL2 R03 36000 R 24820 R C MX09 130 R09 UL1 T09 DL2 R04 36000 R 24820 L C MX10 130 R10 UL1 T10 DL2

R05 36000 R 24860 R C MX11 130 R11 UL1 T11 DL2 R06 36000 R 24860 L C MX12 130 R12 UL1 T12 DL2 R07 36000 R 24900 R C MX13 130 R13 UL1 T13 DL2 R08 36000 R 24900 L C MX14 130 R14 UL1 T14 DL2 R09 36000 R 24940 R C MX15 130 R15 UL1 T15 DL2 R10 36000 R 24940 L C MX16 130 R16 UL1 T16 DL2 R11 36000 R 24980 R C MX17 130 R17 UL1 T17 DL2 R12 36000 R 24980 L C MX18 130 R18 UL1 T18 DL2 R13 36000 R 25020 R C MX19 130 R19 UL1 T19 DL2 R14 36000 R 25020 L C MX20 130 R20 UL1 T20 DL2 R15 36000 R 25060 R C MX21 130 R21 UL1 T21 DL2 R16 36000 R 25060 L C MX22 130 R22 UL1 T22 DL2 R17 36000 R 25100 R C MX23 130 R23 UL1 T23 DL2 R18 36000 R 25100 L C MX24 130 R24 UL1 T24 DL2 R19 36000 R 25140 R C LA01 130 R01 UL1 T01 DL3 R20 36000 R 25140 L C LA02 130 R02 UL1 T02 DL3 R21 36000 R 25180 R C LA03 130 R03 UL1 T03 DL3 R22 36000 R 25180 L C LA04 130 R04 UL1 T04 DL3 R23 36000 R 25220 R C LA05 130 R05 UL1 T05 DL3 R24 36000 R 25220 L C LA06 130 R06 UL1 T06 DL3 R19A 24000 R 25134 R C LA07 130 R07 UL1 T07 DL3 R20A 24000 R 25134 L C LA08 130 R08 UL1 T08 DL3 CMD1 1000 R 24751 R T LA09 130 R09 UL1 T09 DL3 CMD2 1000 R 25249 R T LA10 130 R10 UL1 T10 DL3 CMD3 1000 R 25249 L T LA11 130 R11 UL1 T11 DL3 TLM1 1000 T 17301 R T LA12 130 R12 UL1 T12 DL3 TLM2 1000 T 17302 L T LA13 130 R13 UL1 T13 DL3 LA14 130 R14 UL1 T14 DL3 LA15 130 R15 UL1 T15 DL3 LA16 130 R16 UL1 T16 DL3 LA17 130 R17 UL1 T17 DL3 LA18 130 R18 UL1 T18 DL3 LA19 130 R19 UL1 T19 DL3 LA20 130 R20 UL1 T20 DL3 LA21 130 R21 UL1 T21 DL3 LA22 130 R22 UL1 T22 DL3 LA23 130 R23 UL1 T23 DL3 LA24 130 R24 UL1 T24 DL3 CMDA CMD1 UL1

CMDB CMD2 UL1 CMDC CMD3 UL1 TLMA TLM1 DL1 TLMB TLM2 DL1

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 36M0G7W 36000 4 34800 0.58 3.8 23 DTH2 36M0G7W 36000 8 74170 0.824 11.5 23 DTH3 36M0G7W 36000 8 52190 0.58 7.7 23 DTH4 24M0G7W 24000 4 30300 0.5 7.6 23

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 10 23 CMD 1M00F9D 1000 1 10 23

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) AM01 AM18 DTH3 1 65.2 7.2 10.5 60 60 17.2 AM19 AM20 DTH4 1 65.2 7.2 10.5 60 60 17.2 MX01 MX24 DTH2 1 65.2 7.2 10.5 60 60 -118 17.2 LA01 LA24 DTH 1 65.2 7.2 10.5 59.8 59.8 -118 20.7 CMDA CMDC CMD 1 65.2 -0.7 18.3 TLMA TLMB TLM 1 15 15 40

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 3550 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2450 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6000 48 0.6 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 300 7.5 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 80 8.5 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): 16000 16000 16000 16000 Bus (Watts): (b): (g): (l): (q): 1800 700 1800 700 Total (Watts): (c): (h): (m): (r): 17800 16700 17800 16700 Solar Array (Watts): (d): (i): (n): (s): 22000 19650 18500 17200 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: 2006-09-11 12:02:10
Document Modified: 2006-09-11 12:02:10
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