Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20080930-00194 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2008093000194_668959

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: ATCONTACT77 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: 69 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: 17250 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) 28.6 G 29.1 G R Fixed Satellite Service 18.8 G 19.3 G 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: 77.4 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) 1 S AAB

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) KTR T 48 45 0.05 30 Y 1 2 31.6 63 KRR R 46.5 43.5 0.05 30 Y 1 504 19.5 -116.2 20 1 KTB T 18.5 15.5 0.1 30 N 1 2 31.6 33.5 KRB R 18.5 15.5 0.1 30 N 1 504 -8.5 -116.2 20 1 TLM T 48 45 0.05 30 N 1 2 0.25 42 CMD R 46.5 43.5 0.05 30 N 1 504 19.5 -116.2 TLM T -3 -3 0.05 30 N 1 3 1 -3 CMD R -2 -2 0.05 30 N 1 1154 -32.6 -116.2

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) KTR T C -77.4 ATCONTACT77 KTRC.gxt -119 -118 -118 -118 -118 KTR T X -77.4 ATCONTACT77 KTRX.gxt KRR R C -77.4 ATCONTACT77 KRRC.gxt KRR R X -77.4 ATCONTACT77 KRRX.gxt KTB T C -77.4 ATCONTACT77 KTBC.gxt -119 -119 -118 -118 -118 KTB T X -77.4 ATCONTACT77 KTBX.gxt KRB R C -77.4 ATCONTACT77 KRBC.gxt KRB R X -77.4 ATCONTACT77 KRBX.gxt TLM T C -77.4 ATCONTACT77 TLMC.gxt -120 -119 -118 -118 -118 TLM T X -77.4 ATCONTACT77 TLMX.gxt CMD R C -77.4 ATCONTACT77 CMDC.gxt CMD R X -77.4 ATCONTACT77 CMDX.gxt TLM T C -77.4 TLM T X -77.4 CMD R C -77.4 CMD R X -77.4

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) BR1 2000 R 29096 R T SOS1 SOS1 CMD BT1 2000 T 19296 L T TO1 SOS1 CMDO SOS1 2000 R 29098 R T SOS2 SOS2 TLM SOS2 2000 T 19298 L T TO2 SOS2 TLMO KR017 125000 R 28662.5 L C BR1 BR1 KRB KR018 125000 R 28787.5 L C BT1 BT1 KTB KR019 125000 R 28912.5 L C CR17 KR017 KRR KR020 125000 R 29037.5 L C CR18 KR018 KRR KR021 125000 R 28662.5 R C CR19 KR019 KRR KR022 125000 R 28787.5 R C CR20 KR020 KRR KR023 125000 R 28912.5 R C CR21 KR021 KRR KR024 125000 R 29037.5 R C CR22 KR022 KRR KT009 250000 T 18925 L C CR23 KR023 KRR KT010 250000 T 19175 L C CR24 KR024 KRR KT011 250000 T 18925 R C CT09 KT009 KTR KT012 250000 T 19175 R C CT10 KT010 KTR CT11 KT011 KTR CT12 KT012 KTR

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) COMT1 250MG7W 250000 4 224000 0.67 5.4 17.6 COMR1 3M50G7W 3500 4 2520 0.4 7.1 19.1 BT1 334KG7D 334 4 200 0.4 4.2 16.2 BR1 8K00G7D 8 4 5 0.4 4.2 16.2 SOST1 2M00G7D 2000 2 1000 1 15 27 SOSR1 1M00G7D 1000 2 500 1 15 27 COMT2 125MG7W 125000 4 74000 0.45 6.3 18.5 COMR2 7M00G7W 7000 4 10100 0.9 9.3 21.5 COMR3 700KG2W 700 4 500 0.4 7.1 19.1

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) SOS3 4K00F9D 4 FDM/FM 18 27

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) CT09 CT12 COMT1 1 41 63 63 16 CR17 CR24 COMR1 34 3600 44.6 2.8 2.8 47.4 47.4 SOS1 SOS1 SOSR1 59 17 17 77 77 SOS2 SOS2 SOST1 55.5 42 42 28.9 TO1 TO1 SOS3 68.9 21.1 21.1 90 90 TO2 TO2 SOS3 65.3 -3 -3 39.7 CT09 CT12 COMT2 1 41 63 63 -121 14.6 CR17 CR24 COMR2 17 7200 49.3 5 5 54.3 54.3 CR17 CR24 COMR3 40 720 44.6 2.8 2.8 47.4 47.4

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 2508 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 0 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3154 4.8 0.78 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 646 2.5 0.93 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 38 2.5 0.72 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): 8600 8170 7050 6696 Bus (Watts): (b): (g): (l): (q): 2100 2000 1720 1639 Total (Watts): (c): (h): (m): (r): 10700 10170 8770 8335 Solar Array (Watts): (d): (i): (n): (s): 11200 10670 9180 8745 Depth of Battery (e) (j) (o) (t) Discharge (%): 70 % 70 % 70 % 70 % 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? X YES NO 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: 2008-10-07 10:32:16
Document Modified: 2008-10-07 10:32:16
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