Attachment Sched S Tech Report

This document pretains to SAT-LOA-20110809-00156 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2011080900156_911500

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 97W 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: 48 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: 1920 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 f. Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode 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 19.7 G 20.2 G T Fixed Satellite Service 19.7 G 20.2 G T Direct to Home in the Fixed Fixed Satellite Service 29.5 G 30.0 G R 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: 97.1 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 Angle (o) Other Plane (Seconds) Node (Deg.) (Degrees) 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 + Hawaii LABC S Uplink beam centered on Los Angeles, CA CRBC S Uplink beam centered on Castle Rock, 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) Input (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Losses Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) (dB) Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dBW) Temp (k) (db/K) (dBW/m2) UL1 R 50.7 49.7 0.1 30 Y LABC 1862 18 -105 20 1 UL2 R 51.2 50.2 0.1 30 Y CRBC 1862 18.5 -105 20 1 DL1 T 37.3 29.3 0.1 30 Y CONUS+ 2.4 148 59

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 -97.1 LA RX_CO.gxt UL2 R C -97.1 CRK RX_CO.gxt DL1 T C -97.1 TX_CO.gxt -124 -124 -124 -124 -124

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 (T ID Gain (dB) No. ID No. or C) R0001 36000 R 28375 R C N42 121 R0042 UL2 T0042 DL1 R0002 36000 R 28375 L C N43 121 R0043 UL2 T0043 DL1 R0003 36000 R 28415 R C N44 121 R0044 UL2 T0044 DL1 R0004 36000 R 28415 L C N45 121 R0045 UL2 T0045 DL1 R0005 36000 R 28455 R C N46 121 R0046 UL2 T0046 DL1 R0006 36000 R 28455 L C N47 121 R0047 UL2 T0047 DL1 R0007 36000 R 28495 R C N48 121 R0048 UL2 T0048 DL1 R0008 36000 R 28495 L C CMD1 CMD1 UL2 R0009 36000 R 28535 R C CMD2 CMD2 UL2 R0010 36000 R 28535 L C TLM1 TLM1 DL1 R0011 36000 R 28575 R C TLM2 TLM2 DL1 R0012 36000 R 28575 L C N1 121 R0001 UL1 T0001 DL1 R0013 36000 R 29275 R C N2 121 R0002 UL1 T0002 DL1 R0014 36000 R 29275 L C N3 121 R0003 UL1 T0003 DL1 R0015 36000 R 29315 R C N4 121 R0004 UL1 T0004 DL1 R0016 36000 R 29315 L C N5 121 R0005 UL1 T0005 DL1 R0017 36000 R 29355 R C N6 121 R0006 UL1 T0006 DL1 R0018 36000 R 29355 L C N7 121 R0007 UL1 T0007 DL1 R0019 36000 R 29395 R C N8 121 R0008 UL1 T0008 DL1 R0020 36000 R 29395 L C N9 121 R0009 UL1 T0009 DL1 R0021 36000 R 29435 R C N10 121 R0010 UL1 T0010 DL1 R0022 36000 R 29435 L C N11 121 R0011 UL1 T0011 DL1 R0023 36000 R 29475 R C N12 121 R0012 UL1 T0012 DL1 R0024 36000 R 29475 L C N13 121 R0013 UL1 T0013 DL1 R0025 36000 R 29530 R C N14 121 R0014 UL1 T0014 DL1 R0026 36000 R 29530 L C N15 121 R0015 UL1 T0015 DL1 R0027 36000 R 29570 R C N16 121 R0016 UL1 T0016 DL1 R0028 36000 R 29570 L C N17 121 R0017 UL1 T0017 DL1 R0029 36000 R 29610 R C N18 121 R0018 UL1 T0018 DL1 R0030 36000 R 29610 L C N19 121 R0019 UL1 T0019 DL1

R0031 36000 R 29650 R C N20 121 R0020 UL1 T0020 DL1 R0032 36000 R 29650 L C N21 121 R0021 UL1 T0021 DL1 T0033 36000 T 19890 R C N22 121 R0022 UL1 T0022 DL1 T0034 36000 T 19890 L C N23 121 R0023 UL1 T0023 DL1 T0035 36000 T 19930 R C N24 121 R0024 UL1 T0024 DL1 T0036 36000 T 19930 L C N25 121 R0025 UL2 T0025 DL1 T0037 36000 T 19970 R C N26 121 R0026 UL2 T0026 DL1 T0038 36000 T 19970 L C N27 121 R0027 UL2 T0027 DL1 T0039 36000 T 20010 R C N28 121 R0028 UL2 T0028 DL1 T0040 36000 T 20010 L C N29 121 R0029 UL2 T0029 DL1 T0041 36000 T 20050 R C N30 121 R0030 UL2 T0030 DL1 T0042 36000 T 20050 L C N31 121 R0031 UL2 T0031 DL1 T0043 36000 T 20090 R C N32 121 R0032 UL2 T0032 DL1 T0044 36000 T 20090 L C N33 121 R0033 UL2 T0033 DL1 T0045 36000 T 20130 R C N34 121 R0034 UL2 T0034 DL1 T0046 36000 T 20130 L C N35 121 R0035 UL2 T0035 DL1 T0047 36000 T 20170 R C N36 121 R0036 UL2 T0036 DL1 T0048 36000 T 20170 L C N37 121 R0037 UL2 T0037 DL1 TLM1 106 T 19701 L T N38 121 R0038 UL2 T0038 DL1 TLM2 106 T 19702 L T N39 121 R0039 UL2 T0039 DL1 R0033 36000 R 29690 R C N40 121 R0040 UL2 T0040 DL1 R0034 36000 R 29690 L C N41 121 R0041 UL2 T0041 DL1 R0035 36000 R 29730 R C R0036 36000 R 29730 L C R0037 36000 R 29770 R C R0038 36000 R 29770 L C R0039 36000 R 29810 R C R0040 36000 R 29810 L C R0041 36000 R 29850 R C R0042 36000 R 29850 L C R0043 36000 R 29890 R C R0044 36000 R 29890 L C R0045 36000 R 29930 R C R0046 36000 R 29930 L C R0047 36000 R 29970 R C R0048 36000 R 29970 L C T0001 36000 T 18330 R C T0002 36000 T 18330 L C T0003 36000 T 18370 R C

T0004 36000 T 18370 L C T0005 36000 T 18410 R C T0006 36000 T 18410 L C T0007 36000 T 18450 R C T0008 36000 T 18450 L C T0009 36000 T 18490 R C T0010 36000 T 18490 L C T0011 36000 T 18530 R C T0012 36000 T 18530 L C T0013 36000 T 18570 R C T0014 36000 T 18570 L C T0015 36000 T 18610 R C T0016 36000 T 18610 L C T0017 36000 T 18650 R C T0018 36000 T 18650 L C T0019 36000 T 18690 R C T0020 36000 T 18690 L C T0021 36000 T 18730 R C T0022 36000 T 18730 L C T0023 36000 T 18770 R C T0024 36000 T 18770 L C T0025 36000 T 19730 R C T0026 36000 T 19730 L C T0027 36000 T 19770 R C T0028 36000 T 19770 L C T0029 36000 T 19810 R C T0030 36000 T 19810 L C T0031 36000 T 19850 R C T0032 36000 T 19850 L C CMD1 1300 R 29502 L T CMD2 1300 R 29998 L T

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) M1 36M0G7W 36000 4 38720 0.645 4.7 16.9

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) C1 1M30F9D 1300 1 15 27.2 T1 106KG9D 106 1 14 26.2

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. Power (o)Assoc. Transponder (kHz) No.) Bandwidth (Table S11) (Table S12) Stn. Max. Power (dBW) Flux Density Stn Rec. (a) Start (b) End (kHz) Antenna (dBW/m2/Hz) G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dB/K) N1 N48 M1 1 66.9 9.3 14.3 51 59 -118.9 18.5 TLM1 TLM2 T1 1 15.3 15.3 -146.7 41.8 CMD1 CMD2 C1 1 66.9 4.1 20.1

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 36 0.6 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 266 16 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 104 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): 19200 19200 19200 19200 Bus (Watts): (b): (g): (l): (q): 1800 700 1800 700 Total (Watts): (c): (h): (m): (r): 21000 19900 21000 19900 Solar Array (Watts): (d): (i): (n): (s): 26308 23486 22174 20600 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?: 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: 2011-08-10 13:57:53
Document Modified: 2011-08-10 13:57:53
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