Attachment Sched S Tech Report

This document pretains to SAT-LOA-20100217-00029 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2010021700029_801788

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: VIASAT-89W N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 16 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: 1760 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) 28100 M 28600 M R Fixed Satellite Service 29500 M 30000 M R Fixed Satellite Service 18300 M 18800 M T Fixed Satellite Service 19700 M 20200 M 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: 89.1 W See main narrative. 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) SA1 S -6 dB contour of the uplink CONUS beam. SA2 S -6 dB contour of the downlink CONUS beam. SA3 S -6 dB contour of the uplink South American beam. SA4 S -6 dB contour of the downlink South American beam. SA5 S Visible Earth.

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) NAR R 35.5 29.5 0.12 0.12 30 N SA1 795 6.5 -98.2 25 1 SAR R 35.5 29.5 0.12 0.12 30 N SA3 795 6.5 -98.2 25 1 SARL R 35.5 29.5 0.12 0.12 30 N SA3 795 6.5 -98.2 25 1 NATL T 35 29 0.12 0.12 30 N SA2 1 417 61.2 SAT T 35 29 0.12 0.12 30 N SA4 1 417 61.2 SATL T 35 29 0.12 0.12 30 N SA4 1 417 61.2 OMNI R 3 0 0.12 0.12 30 N SA5 1585 -29 OMNI T 3 0 0.12 0.12 30 N SA5 3 12.6 14

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) NAR R C -89.1 NARR.gxt SAR R C -89.1 SARR.gxt SARL R C -89.1 SARL.gxt NATL T C -89.1 NATL.gxt -143.1 -139.2 -135.4 -130.2 -126.5 SAT T C -89.1 SATR.gxt -133.6 -131.9 -129.7 -127.4 -125.2 SATL T C -89.1 SATL.gxt -133.6 -131.9 -129.7 -127.4 -125.2 OMNI T C -89.1 -144.1 -144.1 -144.1 -144.1 -144.1

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) UL01 110000 R 28164 R C T0001 139.5 UL01 NARR DL01 NATL UL02 110000 R 28286 R C T0002 139.5 UL02 NARR DL02 NATL UL03 110000 R 28414 R C T0003 139.5 UL03 NARR DL03 NATL UL04 110000 R 28538 R C T0004 139.5 UL04 NARR DL04 NATL UL05 110000 R 28164 L C T0005 139.5 UL05 SARL DL05 SATR UL06 110000 R 28286 L C T0006 139.5 UL06 SARL DL06 SATR UL07 110000 R 28414 L C T0007 139.5 UL07 SARL DL07 SATR UL08 110000 R 28538 L C T0008 139.5 UL08 SARL DL08 SATR UL09 110000 R 29567 R C T0009 139.5 UL01 NARR DL05 SATR UL10 110000 R 29689 R C T0010 139.5 UL02 NARR DL06 SATR UL11 110000 R 29811 R C T0011 139.5 UL03 NARR DL07 SATR UL12 110000 R 29933 R C T0012 139.5 UL04 NARR DL08 SATR UL13 110000 R 29567 L C T0013 139.5 UL05 SARL DL01 NATL UL14 110000 R 29689 L C T0014 139.5 UL06 SARL DL02 NATL UL15 110000 R 29811 L C T0015 139.5 UL07 SARL DL03 NATL UL16 110000 R 29933 L C T0016 139.5 UL08 SARL DL04 NATL DL01 110000 T 18364 L C T0017 139.9 UL09 SARR DL09 SATL DL02 110000 T 18486 L C T0018 139.9 UL10 SARR DL10 SATL DL03 110000 T 18614 L C T0019 139.9 UL11 SARR DL11 SATL DL04 110000 T 18736 L C T0020 139.9 UL12 SARR DL12 SATL DL05 110000 T 18364 R C T0021 139.9 UL13 SARL DL13 SATR DL06 110000 T 18486 R C T0022 139.9 UL14 SARL DL14 SATR DL07 110000 T 18614 R C T0023 139.9 UL15 SARL DL15 SATR DL08 110000 T 18736 R C T0024 139.9 UL16 SARL DL16 SATR DL09 110000 T 19767 L C CMD1 CMD1 NARR DL10 110000 T 19889 L C CMD2 CMD2 NARR DL11 110000 T 20011 L C CMD3 CMD1 OMNIR DL12 110000 T 20133 L C CMD4 CMD2 OMNIR DL13 110000 T 19767 R C TLM1 TLM1 NATL DL14 110000 T 19889 R C TLM2 TLM2 NATL

DL15 110000 T 20011 R C TLM3 TLM1 OMNIL DL16 110000 T 20133 R C TLM4 TLM2 OMNIL CMD1 1000 R 28597 R T CMD2 1000 R 28599 R T TLM1 1000 T 18797 L T TLM2 1000 T 18799 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) D1 110MG7D 110000 4 1217680 0.797 5.1 17.3 D2 110MG7D 110000 8 2032480 0.8869 11.2 23.4 D3 2M75G7D 2750 4 2853 0.747 4.4 16.6 D4 2M07G7D 2065 4 1905 0.6642 3.5 15.7 D5 1M38G7D 1380 4 952.5 0.497 1.4 13.6 D6 900KG7D 900 2 312.5 0.5 -0.4 11.8

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. 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) A1 1M00F2D 1000 1 10 22.2 A2 1M00G2D 1000 1 9 21.2

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. (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 T0016 D1 1 LB1.doc 64.9 10.2 16.2 55.2 61.2 -120.7 18.4 T0001 T0016 D2 1 LB2.doc 64.9 10.2 16.2 55.2 61.2 -120.7 38 T0001 T0016 D3 34 3235 LB3.doc 47.1 4 7 34.9 40.9 -125 38 T0001 T0016 D4 46 2391 LB4.doc 47.1 2.7 5.7 33.6 39.6 -125.1 38 T0001 T0016 D5 69 1594 LB5.doc 44.1 1 4 31.8 37.8 -125.1 38 T0001 T0016 D6 106 1037 LB6.doc 44.1 -1 2 29.9 35.9 -125.1 38 T0017 T0024 D1 1 LB7.doc 65.3 9.8 15.8 55.2 61.2 -121 19 T0017 T0024 D2 1 LB8.doc 65.3 9.8 15.8 55.2 61.2 -121 38.6 T0017 T0024 D3 34 3235 LB9.doc 47.6 4 7 34.9 40.9 -125.3 38.6 T0017 T0024 D4 46 2391 LB10.doc 47.6 2.7 5.7 33.6 39.6 -125.4 38.6 T0017 T0024 D5 69 1594 LB11.doc 44.5 1 4 31.8 37.8 -125.4 38.6 T0017 T0024 D6 106 1037 LB12.doc 44.5 -1 2 29.9 35.9 -125.4 38.6 CMD1 CMD2 A1 1 CMD1.doc 64.9 -14.6 1.4 6.5 CMD3 CMD4 A1 1 CMD2.doc 66.8 15.5 20.5 -29 TLM1 TLM2 A2 1 TLM1.doc 21 27 -131.3 38 TLM3 TLM4 A2 1 TLM2.doc 11 14 -144.1 44

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 3350 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 5193 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 8543 8.6 0.882 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1560 4.3 0.858 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 86.7 8.6 0.757 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): 14560 14560 14560 14560 Bus (Watts): (b): (g): (l): (q): 2500 1350 2500 1350 Total (Watts): (c): (h): (m): (r): 17060 15910 17060 15910 Solar Array (Watts): (d): (i): (n): (s): 22596 20174 20357 18340 Depth of Battery (e) (j) (o) (t) Discharge (%): 73.2 % % 76.3 % % 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: 2010-02-18 09:31:51
Document Modified: 2010-02-18 09:31:51
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