Attachment Schedule S Tech Data

This document pretains to SAT-LOA-20040917-00182 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2004091700182_406459

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: RAINBOW 4 9/1/2010 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 9/1/2006 15 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 9/1/2008 32 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: 6/1/2010 6/30/2010 768 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) 12.2 G 12.7 G T Broadcasting Satellite Service - Video 17.3 G 17.8 G R Feeder Link for Broadcasting Satellite Service in FSS 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: 166 W Orbital location awarded through Auction No. 52 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: 166 W e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 166 W 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) ALASKA S Alaska (ALS00002) HAWAII S Hawaii (HWA00002) WEST USA S Western Contiguous United States (USAPSA02)

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) ALS2 T 38.5 35.3 0.05 0.05 30 N ALASKA 1 30.2 53.3 HWA T 45.7 42.7 0.05 0.05 30 N HAWAII 1 13.5 56.9 USP2 T 40.1 37.1 0.05 0.05 30 N WEST US 1 30.2 54.9 USP R 37.8 34.3 0.05 0.05 30 N WEST US 1184 7.1 -96.2 12 4

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) ALS2 T C -166 166_ALS00002_DN.gxt HWA T C -166 166_HWA00002_DN.gxt USP2 T C -166 166_USAPSA02_DN.gxt USP R C -166 166_USAPSA02_UP.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) 1 24000 T 12224 R C AL001 111.4 1 USPU 1 ALS2 1 24000 R 17324 R C AL002 111.4 2 USPU 2 ALS2 2 24000 R 17338.58 L C AL003 111.4 3 USPU 3 ALS2 2 24000 T 12238.58 L C AL004 111.4 4 USPU 4 ALS2 3 24000 R 17353.16 R C AL005 111.4 5 USPU 5 ALS2 3 24000 T 12253.16 R C AL006 111.4 6 USPU 6 ALS2 4 24000 R 17367.74 L C AL007 111.4 7 USPU 7 ALS2 4 24000 T 12267.74 L C AL008 111.4 8 USPU 8 ALS2 5 24000 R 17382.32 R C AL009 111.4 9 USPU 9 ALS2 5 24000 T 12282.32 R C AL010 111.4 10 USPU 10 ALS2 6 24000 R 17396.90 L C AL011 111.4 11 USPU 11 ALS2 6 24000 T 12296.90 L C AL012 111.4 12 USPU 12 ALS2 7 24000 R 17411.48 R C AL013 111.4 13 USPU 13 ALS2 7 24000 T 12311.48 R C AL014 111.4 14 USPU 14 ALS2 8 24000 R 17426.06 L C AL015 111.4 15 USPU 15 ALS2 8 24000 T 12326.06 L C AL016 111.4 16 USPU 16 ALS2 9 24000 R 17440.64 R C AL017 111.4 17 USPU 17 ALS2 9 24000 T 12340.64 R C AL018 111.4 18 USPU 18 ALS2 10 24000 R 17455.22 L C AL019 111.4 19 USPU 19 ALS2 10 24000 T 12355.22 L C AL020 111.4 20 USPU 20 ALS2 11 24000 R 17439.80 R C AL021 111.4 21 USPU 21 ALS2 11 24000 T 12369.80 R C AL022 111.4 22 USPU 22 ALS2 12 24000 R 17484.38 L C AL023 111.4 23 USPU 23 ALS2 12 24000 T 12384.38 L C AL024 111.4 24 USPU 24 ALS2 13 24000 R 17498.96 R C AL025 111.4 25 USPU 25 ALS2 13 24000 T 12398.96 R C AL026 111.4 26 USPU 26 ALS2 14 24000 R 17513.54 L C AL027 111.4 27 USPU 27 ALS2 14 24000 T 12413.54 L C AL028 111.4 28 USPU 28 ALS2 15 24000 R 17528.12 R C AL029 111.4 29 USPU 29 ALS2 15 24000 T 12428.12 R C AL030 111.4 30 USPU 30 ALS2

16 24000 R 17542.70 L C AL031 111.4 31 USPU 31 ALS2 16 24000 T 12442.70 L C AL032 111.4 32 USPU 32 ALS2 17 24000 R 17557.28 R C US001 111.4 1 USPU 1 USP2 17 24000 T 12457.28 R C US002 111.4 2 USPU 2 USP2 18 24000 R 17571.86 L C US003 111.4 3 USPU 3 USP2 18 24000 T 12471.86 L C US004 111.4 4 USPU 4 USP2 19 24000 R 17586.44 R C US005 111.4 5 USPU 5 USP2 19 24000 T 12486.44 R C US006 111.4 6 USPU 6 USP2 20 24000 R 17601.02 L C US007 111.4 7 USPU 7 USP2 20 24000 T 12501.02 L C US008 111.4 8 USPU 8 USP2 21 24000 R 17615.60 R C US009 111.4 9 USPU 9 USP2 21 24000 T 12515.60 R C US010 111.4 10 USPU 10 USP2 22 24000 R 17630.18 L C US011 111.4 11 USPU 11 USP2 22 24000 T 12530.18 L C US012 111.4 12 USPU 12 USP2 23 24000 R 17644.76 R C US013 111.4 13 USPU 13 USP2 23 24000 T 12544.76 R C US014 111.4 14 USPU 14 USP2 24 24000 R 17659.34 L C US015 111.4 15 USPU 15 USP2 24 24000 T 12559.34 L C US016 111.4 16 USPU 16 USP2 25 24000 R 17673.92 R C US017 111.4 17 USPU 17 USP2 25 24000 T 12573.92 R C US018 111.4 18 USPU 18 USP2 26 24000 R 17688.50 L C US019 111.4 19 USPU 19 USP2 26 24000 T 12588.50 L C US020 111.4 20 USPU 20 USP2 27 24000 R 17703.08 R C US021 111.4 21 USPU 21 USP2 27 24000 T 12603.08 R C US022 111.4 22 USPU 22 USP2 28 24000 R 17717.66 L C US023 111.4 23 USPU 23 USP2 28 24000 T 12617.66 L C US024 111.4 24 USPU 24 USP2 29 24000 R 17732.24 R C US025 111.4 25 USPU 25 USP2 29 24000 T 12632.24 R C US026 111.4 26 USPU 26 USP2 30 24000 R 17746.82 L C US027 111.4 27 USPU 27 USP2 30 24000 T 12646.82 L C US028 111.4 28 USPU 28 USP2 31 24000 R 17761.40 R C US029 111.4 29 USPU 29 USP2 31 24000 T 12661.40 R C US030 111.4 30 USPU 30 USP2 32 24000 R 17775.98 L C US031 111.4 31 USPU 31 USP2 32 24000 T 12675.98 L C US032 111.4 32 USPU 32 USP2 HW001 107.9 1 USPU 1 USP2 HW002 107.9 2 USPU 2 USP2 HW003 107.9 3 USPU 3 USP2 HW004 107.9 4 USPU 4 USP2 HW005 107.9 5 USPU 5 USP2

HW006 107.9 6 USPU 6 USP2 HW007 107.9 7 USPU 7 USP2 HW008 107.9 8 USPU 8 USP2 HW009 107.9 9 USPU 9 USP2 HW010 107.9 10 USPU 10 USP2 HW011 107.9 11 USPU 11 USP2 HW012 107.9 12 USPU 12 USP2 HW013 107.9 13 USPU 13 USP2 HW014 107.9 14 USPU 14 USP2 HW015 107.9 15 USPU 15 USP2 HW016 107.9 16 USPU 16 USP2 HW017 107.9 17 USPU 17 USP2 HW018 107.9 18 USPU 18 USP2 HW019 107.9 19 USPU 19 USP2 HW020 107.9 20 USPU 20 USP2 HW021 107.9 21 USPU 21 USP2 HW022 107.9 22 USPU 22 USP2 HW023 107.9 23 USPU 23 USP2 HW024 107.9 24 USPU 24 USP2 HW025 107.9 25 USPU 25 USP2 HW026 107.9 26 USPU 26 USP2 HW027 107.9 27 USPU 27 USP2 HW028 107.9 28 USPU 28 USP2 HW029 107.9 29 USPU 29 USP2 HW030 107.9 30 USPU 30 USP2 HW031 107.9 31 USPU 31 USP2 HW032 107.9 32 USPU 32 USP2

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) 001 24M0G7W 24000 4 40000 0.58 10 25

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)

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) AL001 AL032 1 1 166 link.xls 50.3 53.3 14.7 HW001 HW032 1 1 166 link.xls 53.9 56.9 11.1 US001 US032 1 1 166 link.xls 51.9 54.9 13.1 UPL 1 1 66.2 13.1 16.5

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): #Error

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 2400 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2400 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 4800 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 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): 7100 7100 7100 7100 Bus (Watts): (b): (g): (l): (q): 800 Total (Watts): (c): (h): (m): (r): 8400 Solar Array (Watts): (d): (i): (n): (s): 9000 Depth of Battery (e) (j) (o) (t) Discharge (%): % % % % 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: 2004-11-24 13:35:10
Document Modified: 2004-11-24 13:35:10
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