Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20090807-00085 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2009080700085_741433

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 RB-2A 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: 72 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: 2592 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 25.15 G R Feeder Link for Broadcasting Satellite Service in FSS 17.3 G 17.7 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: 102.765 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 0.025 Degrees Tolerance: g. Westernmost: e. Toward East: 0.025 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) AK S Alaska WA S Seattle and surrounding area UT S Salt Lake City and surrounding area TX S El Paso and surrounfing area NWUF S Moxee, WA and surrounding area CONUS S Conus

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 52 49 0.1 25 Y NWUF 1417 20.5 -94 20 1 DL1 T 47.2 41.2 0.1 25 Y AK 1.2 27.5 55.6 DL2 T 47.4 41.4 0.1 25 Y WA 3.5 6.6 55.6 DL3 T 47.5 41.5 0.1 25 Y UT 3.7 6.5 55.6 DL4 T 47.8 41.8 0.1 25 Y TX 4.1 6 55.6 CMD R 38.5 37.5 0.1 27 N CONUS 17783 -4 TLM T 24 22 0.1 27 N CONUS 2 14.4 35.6

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 -102.8 DIRECTV RB-2 RX1.gxt DL1 T C -102.8 DIRECTV RB-2 TX1.gxt DL2 T C -102.8 DIRECTV RB-2 TX2.gxt DL3 T C -102.8 DIRECTV RB-2 TX3.gxt DL4 T C -102.8 DIRECTV RB-2 TX4.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 17345 R C UT011 150 R11 UL1 T11 DL3 T02 36000 T 17345 L C UT012 150 R12 UL1 T12 DL3 T03 36000 T 17385 R C UT013 150 R13 UL1 T13 DL3 T04 36000 T 17385 L C UT014 150 R14 UL1 T14 DL3 T05 36000 T 17425 R C UT015 150 R15 UL1 T15 DL3 T06 36000 T 17425 L C UT016 150 R16 UL1 T16 DL3 T07 36000 T 17465 R C UT017 150 R17 UL1 T17 DL3 T08 36000 T 17465 L C UT018 150 R18 UL1 T18 DL3 T09 36000 T 17505 R C TX001 150 R01 UL1 T01 DL4 T10 36000 T 17505 L C TX002 150 R02 UL1 T02 DL4 T11 36000 T 17545 R C TX003 150 R03 UL1 T03 DL4 T12 36000 T 17545 L C TX004 150 R04 UL1 T04 DL4 T13 36000 T 17585 R C TX005 150 R05 UL1 T05 DL4 T14 36000 T 17585 L C TX006 150 R06 UL1 T06 DL4 T15 36000 T 17625 R C TX007 150 R07 UL1 T07 DL4 T16 36000 T 17625 L C TX008 150 R08 UL1 T08 DL4 T17 36000 T 17665 R C TX009 150 R09 UL1 T09 DL4 T18 36000 T 17665 L C TX010 150 R10 UL1 T10 DL4 R01 36000 R 24785 R C TX011 150 R11 UL1 T11 DL4 R02 36000 R 24785 L C TX012 150 R12 UL1 T12 DL4 R03 36000 R 24825 R C TX013 150 R13 UL1 T13 DL4 R04 36000 R 24825 L C TX014 150 R14 UL1 T14 DL4 R05 36000 R 24865 R C TX015 150 R15 UL1 T15 DL4 R06 36000 R 24865 L C TX016 150 R16 UL1 T16 DL4 R07 36000 R 24905 R C TX017 150 R17 UL1 T17 DL4 R08 36000 R 24905 L C TX018 150 R18 UL1 T18 DL4 R09 36000 R 24945 R C CMD1 CMD1 CMD R10 36000 R 24945 L C CMD2 CMD2 CMD R11 36000 R 24985 R C TLM1 TLM1 TLM R12 36000 R 24985 L C TLM2 TLM2 TLM

R13 36000 R 25025 R C AK001 150 R01 UL1 T01 DL1 R14 36000 R 25025 L C AK002 150 R02 UL1 T02 DL1 R15 36000 R 25065 R C AK003 150 R03 UL1 T03 DL1 R16 36000 R 25065 L C AK004 150 R04 UL1 T04 DL1 R17 36000 R 25105 R C AK005 150 R05 UL1 T05 DL1 R18 36000 R 25105 L C AK006 150 R06 UL1 T06 DL1 CMD1 1300 R 29255 L T AK007 150 R07 UL1 T07 DL1 CMD2 1300 R 29497 L T AK008 150 R08 UL1 T08 DL1 TLM1 106 T 18302.25 R T AK009 150 R09 UL1 T09 DL1 TLM2 106 T 18302.75 L T AK010 150 R10 UL1 T10 DL1 AK011 150 R11 UL1 T11 DL1 AK012 150 R12 UL1 T12 DL1 AK013 150 R13 UL1 T13 DL1 AK014 150 R14 UL1 T14 DL1 AK015 150 R15 UL1 T15 DL1 AK016 150 R16 UL1 T16 DL1 AK017 150 R17 UL1 T17 DL1 AK018 150 R18 UL1 T18 DL1 WA001 150 R01 UL1 T01 DL2 WA002 150 R02 UL1 T02 DL2 WA003 150 R03 UL1 T03 DL2 WA004 150 R04 UL1 T04 DL2 WA005 150 R05 UL1 T05 DL2 WA006 150 R06 UL1 T06 DL2 WA007 150 R07 UL1 T07 DL2 WA008 150 R08 UL1 T08 DL2 WA009 150 R09 UL1 T09 DL2 WA010 150 R10 UL1 T10 DL2 WA011 150 R11 UL1 T11 DL2 WA012 150 R12 UL1 T12 DL2 WA013 150 R13 UL1 T13 DL2 WA014 150 R14 UL1 T14 DL2 WA015 150 R15 UL1 T15 DL2 WA016 150 R16 UL1 T16 DL2 WA017 150 R17 UL1 T17 DL2 WA018 150 R18 UL1 T18 DL2 UT001 150 R01 UL1 T01 DL3 UT002 150 R02 UL1 T02 DL3 UT003 150 R03 UL1 T03 DL3

UT004 150 R04 UL1 T04 DL3 UT005 150 R05 UL1 T05 DL3 UT006 150 R06 UL1 T06 DL3 UT007 150 R07 UL1 T07 DL3 UT008 150 R08 UL1 T08 DL3 UT009 150 R09 UL1 T09 DL3 UT010 150 R10 UL1 T10 DL3

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 16

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 106KG9D 106 1 5.5 17.7 CMD 1M30F9D 1300 1 9.5 21.7

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) UT001 UT018 DTH 1 66.3 1.6 7.6 49.6 55.6 -122 18 TX001 TX018 DTH 1 66.3 1.6 7.6 49.6 55.6 -122 18 WA001 WA018 DTH 1 66.3 1.6 7.6 49.6 55.6 -122 18 AK001 AK018 DTH 1 66.3 1.6 7.6 55.6 61.6 -116 21.8 CMD1 CMD2 CMD 1 66.3 23.7 23.7 90 90 TLM1 TLM2 TLM 1 24 -5.9 11.6 18.1 35.6 -126.4 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 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 Angele CA 90810 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 310 525 5590

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?: 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: 2009-09-21 09:34:34
Document Modified: 2009-09-21 09:34:34
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