Attachment Schedule S Tech Data

This document pretains to SES-AMD-20070309-00336 for Amended Filing on a Satellite Earth Station filing.

IBFS_SESAMD2007030900336_557799

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: CANSAT-24 11/30/2008 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 3/31/2005 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 8/31/2007 448 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: 11/1/2007 11/30/2007 2240 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) 2180 M 2200 M T Mobile Satellite Service 10.7 M 10.95 G T Feeder Link for Mobile Satellite Service in FSS 11.2 M 11.45 G T Feeder Link for Mobile Satellite Service in FSS 13.75 G 13.753 G R Fixed Satellite Service - Transfer Orbit and Emergency Operations 2000 M 2020 M R Mobile-Satellite Service 12.75 G 13.25 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: 111.1 W TerreStar (ITU designator CANSAT-24) will operate at - Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be 111.1WL that is an available Canadian ITU Appendix N/S Station-Keeping provided (Optional): 30B Ku-Band orbital location and TerreStar will use d. Toward West: Degrees E/W 0.05 Degrees Tolerance: that band for feeder link and TTC.operation. g. Westernmost: e. Toward East: 0.05 Degrees 6 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 E_SD1sa.gxt Conus, Alaska, Canada as required by Canadian Authority SA2 S E_SD2a.gxt Hawaii SA3 S E_SD3prsa.gxt Puerto Rico and US Virgin Islands SAFL S E_SAFL.gxt Conus, Southern Canada OMNI S E_OMSA.gxt Global

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) SU1 R 47 46.2 0.03 21.3 N SA1 331 21.8 -158.2 31 1 SD1 T 48 47.2 0.03 18.8 N SA1 2.3 269 72.3 SU2 R 39.9 38.6 0.03 21.3 N SA2 282 15.4 -152.1 31 1 SD2 T 40.8 39.1 0.03 18.3 N SA2 2.3 107 61.1 SU3 R 43.6 41.5 0.03 21.3 N SA3 417 17.4 -154.8 31 1 SD3 T 43.85 41.43 0.03 18.3 N SA3 2.3 106 64.1 KU1 R 46.7 43.9 0.16 30 N SAFL 617 18.8 -112 36 1 KU1 T 46.4 43.6 0.16 30 N SAFL 2.6 3.8 52.15 CMD R 46.7 43.9 0.16 30 N SAFL 32767 -0.5 -112 TLM T 46.4 43.6 0.16 30 N SAFL 10 0.0034 21.7 BCN T 46.4 43.6 0.16 30 N SAFL 10 0.0046 23 PLT R 46.7 43.9 0.16 30 N SAFL 32767 -0.5 -107 CES R 43.42 28.91 0.16 19 N SA1 982 13.5 -158.2 31 1 CES T 43.42 28.91 0.16 19 N SA1 3.4 0.47 40.1 OMN R 3 -4 0 30 N OMNI 2042 -30.1 -82.3 OMN T 3 -4 0 30 N OMNI 3.39 11 13.41 CES R 43.42 28.91 0.16 19 N SA1 982 13.5 -158.2 31 1

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) SU1 R C -111.1 Terrestar-Composite-Rx-updated3a.gxt SD1 T C -111.1 Terrestar-Composite-Tx-updated3a.gxt SU2 R C -111.1 R_SU2co.gxt SD2 T C -111.1 E_SD2co.gxt SU3 R C -111.1 R_SU3co.gxt SD3 T C -111.1 E_SD3co.gxt KU1 R C -111.1 ku-lv-12750L.gxt KU1 T C -111.1 ku-lv-10700L.gxt -153.7 -153.6 -153.5 -153.4 -153.3 OMN T C -111.1 OMNID.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) KLDU 250000 R 12875 L C FLINK 153 KLDU KU1U SLD SD1 KRDU 250000 R 12875 R C RLINK 145 SRU SU1 KLDD1 KU1D KLDD1 250000 T 10825 L C KRDD1 250000 T 10825 R C KLDD2 250000 T 11325 L C KRDD2 250000 T 11325 R C SLD 10000 T 2190 L C SLU 10000 R 2010 L C SRU 10000 R 2010 R C CMD1 800 R 12751 L T CMD2 800 R 12999 L T TLM1 100 T 11200.5 R T TLM2 100 T 11449.5 R T ELOU1 800 R 13750.5 L T ELOU2 800 R 13752.5 L T BEAC 0.001 T 11448 R T PILOT 0.001 T 12992 L T CES 50 T 2190 L C CES 50 R 2010 R C

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) CDMAR 1M25G7W 1250 4 63 0.2 -2.98 -3.484154 CDMAR 1M25G7W 1250 4 5.64 0.2 -2.98 -13.96477 GMR1R 31K3G7W 31.25 4 35.1 0.75 5.5 17.97154 GMR1R 156KG7W 156.25 4 156 0.67 4.4 16.87154 FDMAR 6K50G7W 6.5 4 5.64 0.58 3.4 15.87154 FDMAR 26K0G7W 26 12 38.9 0.5 7.4 19.87154 GMR2R 50K0G7W 50 4 45.1 0.67 4.4 16.87154 GMR2R 200KG7W 200 4 180.7 0.68 4.4 16.87154 OFDMA 54K7G7W 54.7 12 50.8 0.5 7.4 19.87154 OFDMA 54K7G7W 54.7 4 33.9 0.67 4.4 18.87154 EVDOF 1M25G7W 1250 4 964 0.5 1.51 12.85321 EVDOF 1M25G7W 1250 4 5.64 0.2 -3.53 -14.51477 GMR1F 31K3G7W 31.25 4 35.1 0.75 4.76 17.23154 GMR1F 313KG7W 312.512 12 624 0.67 9.58 22.05154 GMR2F 200KG7W 200 12 361.1 0.67 9.58 22.05154 GMR2F 200KG7W 200 4 180.5 0.67 3.72 16.19154 OFDMF 1M25G7W 1250 12 1445.1 0.67 9.58 22.05154 OFDMF 1M25G7W 1250 4 372.57 0.67 3.72 16.19154 CESF 50K0G7W 50 2 1 38 14.67154 CESR 50K0G7W 50 2 1 26 6.43154 CESPR 50K0G7W 50 2 1 32 12.43154

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 138KGXD 100 PM CMD 700KF9D 1000 FM

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) RLINK RLINK CDMAR 129 1250 LB1.doc 0 -9 -6 -1.32 6.95 -181 34.5 RLINK RLINK GMR1R 13 31.25 LB2.doc 0 -9 -6 9.2 14.5 -164 34.5 RLINK RLINK FDMAR 64 6.5 LB3.doc 0 -9 -6 2.6 8.5 -162 34.5 RLINK RLINK GMR2R 8 50 LB4.doc 0 -9 -6 10.6 14.5 -165 34.5 RLINK RLINK OFDMA 8 43.8 LB5.doc 0 -9 -6 9.7 9.7 -162 34.5 FLINK FLINK EVDOF 1 LB6.doc 61 -12.1 -5.9 52.86 75.1 -112 -28 FLINK FLINK GMR1F 4 31.25 LB7.doc 61 -18.5 -5.9 46.4 73.6 -108 -28 FLINK FLINK GMR2F 1 LB8.doc 61 -13.8 -9.8 52.6 69.9 -110 -28 FLINK FLINK OFDMF 17 10.94 LB9.doc 61 -20 -20 40.7 63.9 -121 -28

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 Remote Control (TT C) Location(s): S14a: Street Address: 133438 Allan Park Rd. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Allan Park ON N4N B8 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 519-371-7490 NEW Remote Control (TT C) Location(s): S14a: Street Address: One Aerojet Way S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: North Las Vegas NV 89030 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 571-223-6604 NEW

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 3801 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 2899 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 6700 32 0.84 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 334.8 26.3 0.84 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 58.25 7.6 0.7 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): 10270 10270 10270 10270 Bus (Watts): (b): (g): (l): (q): 1535 1535 1535 1535 Total (Watts): (c): (h): (m): (r): 13193 11805 12905 10890 Solar Array (Watts): (d): (i): (n): (s): 15808 14218 15560 14020 Depth of Battery (e) (j) (o) (t) Discharge (%): 74 % 0 % 74 % 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? 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: 2007-03-27 16:31:42
Document Modified: 2007-03-27 16:31:42
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