Attachment Schedule S Tech Data

This document pretains to SAT-MOD-20041102-00206 for Modification on a Satellite Space Stations filing.

IBFS_SATMOD2004110200206_403543

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: ECHOSTAR-121W-KUX 9/30/2009 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 9/30/2007 12 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 7/31/2009 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: 8/31/2009 8/31/2009 864 MHz GSO NGSO 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) 13.75 G 14.0 G R Fixed Satellite Service 11.45 G 11.7 G R Direct to Home in the Fixed Fixed Satellite Service 10.95 G 11.2 G R Direct to Home in the Fixed 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: 121 W This orbital location provides high elevation angles to Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be all of North and Central America including Hawaii, N/S Station-Keeping provided (Optional): which is very important for satellite services to large d. Toward West: Degrees Degrees E/W 0.05 Tolerance: numbers of small and inexpensive consumer earth g. Westernmost: e. Toward East: 0.05 Degrees stations, which will be used at Ku-band. The high 0.05 Degrees h. Easternmost: elevation minimizes the risk of signal blockage due to buildings and foliage, and also minimizes the i. Reason for service are selection (Optional): atmospheric and rain attenuation.

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 All visible areas of the Earth. SA2 S CONUS, Hawaii, Puerto Rico, Canada, Mexico

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 Flux Density (Y/N) Value Size (dB) (dBW) Temp (k) Pt. (dBW/m2) UAL R 44.4 41.4 0.12 0 30 N SA1 1000 14.4 -98 15 1 UAR R 44.4 41.4 0.12 0 30 N SA1 1000 14.4 -98 15 1 UBR R 44.4 41.4 0.12 0 30 N SA1 1000 14.4 -98 15 1 UBL R 44.4 41.4 0.12 0 30 N SA1 1000 14.4 -98 15 1 DR T 30.8 26.8 0.12 0 30 N SA2 1.8 89.2 50.3 DL T 30.8 26.8 0.12 0 30 N SA2 1.8 89.2 50.3

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) UAL R C -121 UAL.gxt UAR R C -121 UAR.gxt UBR R C -121 UBR.gxt UBL R C -121 UBL.gxt DR T C -121 DR.gxt -152.6 -151.6 -150.6 -150.1 -150.1 DL T C -121 DL.gxt -152.6 -151.6 -150.6 -150.1 -150.1

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) (c) (d) Center (e) (f) TTC (a) (b) Receive Band Transmit Band Channel Assigned T/R Frequency Polarization or Comm Transponder Transponder (c) Channel (d) Beam (e) Channel (f) Beam ID No. Bandwidth Mode (MHz) (H, V, L, R) Channel ID Gain (dB) No. ID No. (kHz) (T or C) U0001 27000 R 13766.5 L C T0001 120 U0001 UAL D0001 DR U0003 27000 R 13796.5 L C T0003 120 U0003 UAL D0003 DR U0005 27000 R 13826.5 L C T0005 120 U0005 UAL D0005 DR U0007 27000 R 13856.5 L C T0007 120 U0007 UAL D0007 DR U0009 27000 R 13886.5 L C T0009 120 U0009 UAL D0009 DR U0011 27000 R 13916.5 L C T0011 120 U0011 UAL D0011 DR U0013 27000 R 13946.5 L C T0013 120 U0013 UAL D0013 DR U0015 27000 R 13976.5 L C T0015 120 U0015 UAL D0015 DR U0002 27000 R 13773.5 R C T0002 120 U0002 UAR D0002 DL U0004 27000 R 13803.5 R C T0004 120 U0004 UAR D0004 DL U0006 27000 R 13833.5 R C T0006 120 U0006 UAR D0006 DL U0008 27000 R 13863.5 R C T0008 120 U0008 UAR D0008 DL U0010 27000 R 13893.5 R C T0010 120 U0010 UAR D0010 DL U0012 27000 R 13923.5 R C T0012 120 U0012 UAR D0012 DL U0014 27000 R 13953.5 R C T0014 120 U0014 UAR D0014 DL U0016 27000 R 13983.5 R C T0016 120 U0016 UAR D0016 DL U0017 27000 R 13766.5 R C T0017 120 U0017 UBR D0017 DL U0019 27000 R 13796.5 R C T0019 120 U0019 UBR D0019 DL U0021 27000 R 13826.5 R C T0021 120 U0021 UBR D0021 DL U0023 27000 R 13856.5 R C T0023 120 U0023 UBR D0023 DL U0025 27000 R 13886.5 R C T0025 120 U0025 UBR D0025 DL U0027 27000 R 13916.5 R C T0027 120 U0027 UBR D0027 DL U0029 27000 R 13946.5 R C T0029 120 U0029 UBR D0029 DL U0031 27000 R 13976.5 R C T0031 120 U0031 UBR D0031 DL U0018 27000 R 13773.5 L C T0018 120 U0018 UBL D0018 DR U0020 27000 R 13803.5 L C T0020 120 U0020 UBL D0020 DR U0022 27000 R 13833.5 L C T0022 120 U0022 UBL D0022 DR U0024 27000 R 13863.5 L C T0024 120 U0024 UBL D0024 DR U0026 27000 R 13893.5 L C T0026 120 U0026 UBL D0026 DR U0028 27000 R 13923.5 L C T0028 120 U0028 UBL D0028 DR

U0030 27000 R 13953.5 L C T0030 120 U0030 UBL D0030 DR U0032 27000 R 13983.5 L C T0032 120 U0032 UBL D0032 DR D0001 27000 T 10966.5 R C D0003 27000 T 10996.5 R C D0005 27000 T 11026.5 R C D0007 27000 T 11056.5 R C D0009 27000 T 11086.5 R C D0011 27000 T 11116.5 R C D0013 27000 T 11146.5 R C D0015 27000 T 11176.5 R C D0017 27000 T 11466.5 L C D0019 27000 T 11496.5 L C D0021 27000 T 11526.5 L C D0023 27000 T 11556.5 L C D0025 27000 T 11586.5 L C D0027 27000 T 11616.5 L C D0029 27000 T 11646.5 L C D0031 27000 T 11676.5 L C D0018 27000 T 11473.5 R C D0020 27000 T 11503.5 R C D0022 27000 T 11533.5 R C D0024 27000 T 11563.5 R C D0026 27000 T 11593.5 R C D0028 27000 T 11623.5 R C D0030 27000 T 11653.5 R C D0032 27000 T 11683.5 R C D0002 27000 T 10973.5 L C D0004 27000 T 11003.5 L C D0006 27000 T 11033.5 L C D0008 27000 T 11063.5 L C D0010 27000 T 11093.5 L C D0012 27000 T 11123.5 L C D0014 27000 T 11153.5 L C D0016 27000 T 11183.5 L 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) D1 27M0G7W 27000 4 33300 0.691 6 18.2

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. Bandwidth per Carrier NTSC, Weighting SCPC/FM Preemphasis, Objective Objective Companded Baseband Baseband Modulation ID (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) T0001 T0032 D1 1 LB1.doc 62.2 3 18 46.3 50.3 -150.1 17.4

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 2300 (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: 4700 44.1 0.87 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1200 8 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 85.3 5 0.74 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): 9450 9450 9450 9450 Bus (Watts): (b): (g): (l): (q): 1800 1000 1800 1000 Total (Watts): (c): (h): (m): (r): 11250 10450 11250 10450 Solar Array (Watts): (d): (i): (n): (s): 14500 12571 12854 11310 Depth of Battery (e) (j) (o) (t) Discharge (%): 75 % % 75 % % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: 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 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? 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: 2004-11-02 14:14:51
Document Modified: 2004-11-02 14:14:51
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC