Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20061006-00118 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2006100600118_531107

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: AMC-18 1/1/2007 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 8/1/2001 21.5 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 11/1/2006 24 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: 11/1/2006 11/30/2006 864 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) 3700 M 4200 M T Fixed Satellite Service 3700 M 4200 M T 5925 M 6425 M R Fixed Satellite Service 5925 M 6425 M R 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: 104.95 W Availaibility of C-band spectrum at 105W (nominal). 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: W e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 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) CNA E -7 dB gain contour of beams CUH and CUV for the uplink; -8 dB gain contour of beams CDH and CDV for the do

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) CDH T 30.24 22.24 0.15 0 31.3 Y 0 CNA 1.65 12.56 41.23 CDV T 30.51 22.51 0.15 0 30.6 Y 90 CNA 1.68 12.56 41.5 CUH R 31.74 23.74 0.15 0 33.8 Y 0 CNA 583 4.01 -96.01 18 1 CUV R 31.61 23.61 0.15 0 32.6 Y 90 CNA 593 3.96 -95.96 18 1 TC R 10 8 0.15 0 Y CNA 585 -17

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) CDH T C -104.95 ch12_CDH.gxt -153 -152 -151 -150 -149 CDV T C -104.95 ch13_CDV.gxt -153 -152 -151 -150 -149 CUH R C -104.95 ch13_CUH.gxt CUV R C -104.95 ch12_CUV.gxt CDH T X -104.95 ch12_CDH_X.gxt CDV T X -104.95 ch13_CDV_X.gxt CUH R X -104.95 ch13_CUH_X.gxt CUV R X -104.95 ch12_CUV_X.gxt TC R C -104.95 amc18_command_rx_antenna.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) CD001 36000 T 3720 V C C0001 112 CU001 CUH CD001 CDV CD003 36000 T 3760 V C C0003 112 CU003 CUH CD003 CDV CD005 36000 T 3800 V C C0005 112 CU005 CUH CD005 CDV CD007 36000 T 3840 V C C0007 112 CU007 CUH CD007 CDV CD009 36000 T 3880 V C C0009 112 CU009 CUH CD009 CDV CD011 36000 T 3920 V C C0011 112 CU011 CUH CD011 CDV CD013 36000 T 3960 V C C0013 112 CU013 CUH CD013 CDV CD015 36000 T 4000 V C C0015 112 CU015 CUH CD015 CDV CD017 36000 T 4040 V C C0017 112 CU017 CUH CD017 CDV CD019 36000 T 4080 V C C0019 112 CU019 CUH CD019 CDV CD021 36000 T 4120 V C C0021 112 CU021 CUH CD021 CDV CD023 36000 T 4160 V C C0023 112 CU023 CUH CD023 CDV CD002 36000 T 3740 H C C0002 112 CU002 CUV CD002 CDH CD004 36000 T 3780 H C C0004 112 CU004 CUV CD004 CDH CD006 36000 T 3820 H C C0006 112 CU006 CUV CD006 CDH CD008 36000 T 3860 H C C0008 112 CU008 CUV CD008 CDH CD010 36000 T 3900 H C C0010 112 CU010 CUV CD010 CDH CD012 36000 T 3940 H C C0012 112 CU012 CUV CD012 CDH CD014 36000 T 3980 H C C0014 112 CU014 CUV CD014 CDH CD016 36000 T 4020 H C C0016 112 CU016 CUV CD016 CDH CD018 36000 T 4060 H C C0018 112 CU018 CUV CD018 CDH CD020 36000 T 4100 H C C0020 112 CU020 CUV CD020 CDH CD022 36000 T 4140 H C C0022 112 CU022 CUV CD022 CDH CD024 36000 T 4180 H C C0024 112 CU024 CUV CD024 CDH CU001 36000 R 5945 H C TC001 TC TC CU003 36000 R 5985 H C TM001 TM1 CDH CU005 36000 R 6025 H C TM002 TM2 CDV CU007 36000 R 6065 H C CU009 36000 R 6105 H C CU011 36000 R 6145 H C

CU013 36000 R 6185 H C CU015 36000 R 6225 H C CU017 36000 R 6265 H C CU019 36000 R 6305 H C CU021 36000 R 6345 H C CU023 36000 R 6385 H C CU002 36000 R 5965 V C CU004 36000 R 6005 V C CU006 36000 R 6045 V C CU008 36000 R 6085 V C CU010 36000 R 6125 V C CU012 36000 R 6165 V C CU014 36000 R 6205 V C CU016 36000 R 6245 V C CU018 36000 R 6285 V C CU020 36000 R 6325 V C CU022 36000 R 6365 V C CU024 36000 R 6405 V C TC 800 R 6423.5 H T TM1 300 T 3700.5 H T TM2 300 T 4199.5 V 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) A 36M0G7W 36000 4 40000 0.691 6.8 19 B 6M95G1W 6950 4 8000 0.691 6.8 19 C 36M0G7W 36000 8 60000 0.614 9.9 22.1 D 100KG1W 100 4 56 0.691 6.8 19 E 1M35G7W 1350 4 1544 0.691 6.8 19

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) F 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 12 26 G 800KF9D 800 1 10 21 H 300KF9D 300 1 9 21

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) C0001 C0024 A 1 7, 8 53.8 14 32 31.1 41.2 -159.7 22.3 C0001 C0024 B 5 6950 7, 8 53.8 -1.5 16.5 22.1 34.1 -159.9 23.7 C0001 C0024 C 1 9, 10 53.8 14 32 32.3 41.2 -160.2 29.8 C0001 C0024 D 360 100 11, 12 47.8 -14.5 3.5 3.8 15.6 -156.7 22.3 C0001 C0024 E 26 1350 11, 12 47.8 0.7 18.7 17.6 26.9 -159.8 22.3 C0001 C0024 F 1 13, 14 2800 53.2 14.6 32.6 35.3 41.2 -149.6 23.7 TC001 TC001 G 1 15 54.4 10 15 TM001 TM002 H 1 15 10 14 -167.3 33.2

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 Remote Control (TT C) Location(s): S14a: Street Address: Woodbine TT&C S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Mt. Airy MD 21771 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 410-549-4300 E7169 Remote Control (TT C) Location(s): S14a: Street Address: Vernon Valley Spacecraft Ops S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Sussex NJ 07461 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 973-823-6000 WB81 Remote Control (TT C) Location(s): S14a: Street Address: Suite 9A, Leanse Place S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Gibraltar Gibraltar S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 011-350-77025 Remote Control (TT C) Location(s): S14a: Street Address: S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):

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 918 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1163 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2081 14.65 0.92 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 360.41 1.82 0.86 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 23.99 3.79 0.79 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): 1516 1516 1516 1516 Bus (Watts): (b): (g): (l): (q): 924 574 924 574 Total (Watts): (c): (h): (m): (r): 2440 2090 2440 2090 Solar Array (Watts): (d): (i): (n): (s): 3592 3044 2797 2483 Depth of Battery (e) (j) (o) (t) Discharge (%): 58 % % 58 % % 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: 2006-10-11 10:01:51
Document Modified: 2006-10-11 10:01:51
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC