Attachment Sched S Tech Report

This document pretains to SAT-LOI-20110914-00180 for Letter of Intent on a Satellite Space Stations filing.

IBFS_SATLOI2011091400180_917384

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: STAR ONE C3 8/31/2012 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 1/26/2010 16 Years 0 c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 5/16/2012 6 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: 6/25/2012 7/31/2012 432 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 f. Lower Frequency (_Hz) Upper Frequency (_Hz) e. T/R Mode 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 10.95 G 11.2 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: 75 W The Brazilian telecommunications authority has Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be authorized Star One to operate the STAR ONE C3 N/S Station-Keeping provided (Optional): satellite at 75° W.L. d. Toward West: Degrees E/W 0.05 Degrees Tolerance: g. Westernmost: e. Toward East: 0.05 Degrees 0.1 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 Angle (o) Other Plane (Seconds) Node (Deg.) (Degrees) 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 -10 dB contour of beams ANDUH and ANDUV SA2 S -10 dB contour of beams BRAUH and BRAUV SA3 S -10 dB contour of beams ANDDH and ANDDV SA4 S -10 dB contour of beams BRADH and BRADV

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) Input (l) Effective (m) (n) (o) G/T (p) Min. Input Attenuator (dB) ID Mode (c) Peak (d) Edge Error Error Polar Iso- Switch- Equatorial Losses Output Max. System Max. Saturation (Degrees) (Degrees) lation (dB) able? Plane (Degrees) (q) Max. (r) Step (dBi) (dBi) (dB) Power (W) EIRP Noice Gain Pt. Flux Density (Y/N) Value Size (dBW) Temp (k) (db/K) (dBW/m2) AND R 34.43 24.43 0.12 30 N 0 SA1 572 6.9 -110 40 1 AND R 34.43 24.43 0.12 30 N 90 SA1 572 6.9 -110 40 1 BRA R 34.75 24.75 0.12 30 N 0 SA2 508 7.7 -110 40 1 BRA R 34.75 24.75 0.12 30 N 90 SA2 508 7.7 -110 40 1 AND T 32.41 22.41 0.12 30 N 0 SA3 1.4 95.3 52.2 AND T 32.41 22.41 0.12 30 N 90 SA3 1.4 95.3 52.2 BRA T 34.82 24.82 0.12 30 N 0 SA4 1.4 99.5 54.8 BRA T 34.82 24.82 0.12 30 N 90 SA4 1.4 99.5 54.8

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) AND R C -75 ANDUH.gxt AND R C -75 ANDUV.gxt BRA R C -75 BRAUH.gxt BRA R C -75 BRAUV.gxt AND T C -75 ANDDH.gxt -169.3 -169.1 -168 -166.9 -165.8 AND T C -75 ANDDV.gxt -169.3 -168.6 -168 -166.9 -163.8 BRA T C -75 BRADH.gxt -168.3 -167.1 -166 -164.9 -158.7 BRA T C -75 BRADV.gxt -168.3 -167.1 -166 -163.7 -157.8

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 (T ID Gain (dB) No. ID No. or C) U0001 72000 R 13795 H C AA001 139.7 U0001 ANDUH D0001 ANDDV U0002 72000 R 13875 H C AA002 139.7 U0002 ANDUH D0002 ANDDV U0003 72000 R 13955 H C AA003 139.7 U0003 ANDUH D0003 ANDDV U0004 72000 R 13799 V C AA004 139.7 U0004 ANDUV D0004 ANDDH U0005 72000 R 13879 V C AA005 139.7 U0005 ANDUV D0005 ANDDH U0006 72000 R 13959 V C AA006 139.7 U0006 ANDUV D0006 ANDDH D0001 72000 T 10990 V C AB001 139.9 U0001 ANDUH D0001 BRADV D0002 72000 T 11070 V C AB002 139.9 U0002 ANDUH D0002 BRADV D0003 72000 T 11150 V C AB003 139.9 U0003 ANDUH D0003 BRADV D0004 72000 T 10994 H C AB004 139.9 U0004 ANDUV D0004 BRADH D0005 72000 T 11074 H C AB005 139.9 U0005 ANDUV D0005 BRADH D0006 72000 T 11154 H C AB006 139.9 U0006 ANDUV D0006 BRADH BA001 139.4 U0001 BRAUH D0001 ANDDV BA002 139.4 U0002 BRAUH D0002 ANDDV BA003 139.4 U0003 BRAUH D0003 ANDDV BA004 139.4 U0004 BRAUV D0004 ANDDH BA005 139.4 U0005 BRAUV D0005 ANDDH BA006 139.4 U0006 BRAUV D0006 ANDDH

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 445KG7W 445 4 512 0.691 5.7 17.9 D2 1M78G7W 1778 4 2048 0.691 5.7 17.9 D3 6M33G7W 6330 4 8448 0.801 5.8 18 D4 17M9G7W 17900 4 19112 0.641 3.9 16.1 D5 36M0G7W 36000 4 50492 0.841 6.5 18.7 D6 72M0G7W 72000 4 100983 0.841 6.5 18.7

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. Power (o)Assoc. Transponder (kHz) No.) Bandwidth (Table S11) (Table S12) Stn. Max. Power (dBW) Flux Density Stn Rec. (a) Start (b) End (kHz) Antenna (dBW/m2/Hz) G/T Gain (dBi) (j) Min. (k) Max. (l) Min. (m) Max. (dB/K) AA001 AA006 D1 161 445 LB1.doc 54.5 -5.9 4.1 24.5 34.5 -148.1 20.8 AA001 AA006 D2 40 1800 LB2.doc 54.5 -1.7 8.3 23.7 33.7 -154.9 24.3 AA001 AA006 D3 11 6500 LB3.doc 54.5 3.9 13.9 29.3 39.3 -154.8 26.6 AA001 AA006 D4 4 18000 LB4.doc 54.5 8.3 18.3 33.7 43.7 -154.9 22.8 AA001 AA006 D5 2 36000 LB5.doc 54.5 11.3 21.3 36.7 46.7 -154.9 26.6 AA001 AA006 D6 1 LB6.doc 54.5 24.4 30 42.2 52.2 -152.4 22.8 AB001 AB006 D1 161 445 LB7.doc 54.5 -7.5 2.5 24.5 34.5 -148.4 20.8 AB001 AB006 D2 40 1800 LB8.doc 54.5 -1.7 8.3 26.3 36.3 -152.6 24.3 AB001 AB006 D3 11 6500 LB9.doc 54.5 3.9 13.9 31.9 41.9 -152.5 26.6 AB001 AB006 D4 4 18000 LB10.doc 54.5 8.3 18.3 36.3 46.3 -152.6 20.8 AB001 AB006 D5 2 36000 LB11.doc 54.5 11.3 21.3 39.3 49.3 -152.7 26.6 AB001 AB006 D6 1 LB12.doc 54.5 22 30 44.8 54.8 -150.2 22.8 BA001 BA006 D1 161 445 LB13.doc 54.5 -7.8 2.2 17.6 27.6 -154.9 24.3 BA001 BA006 D2 40 1800 LB14.doc 54.5 -1.7 8.3 23.7 33.7 -154.9 24.3 BA001 BA006 D3 11 6500 LB15.doc 54.5 3.9 13.9 29.3 39.3 -154.8 26.6 BA001 BA006 D4 4 18000 LB16.doc 54.5 8.3 18.3 33.7 43.7 -154.9 20.8 BA001 BA006 D5 2 36000 LB17.doc 54.5 11.3 21.3 36.7 46.7 -154.9 26.6 BA001 BA006 D6 1 LB18.doc 54.5 24.4 30 42.2 52.2 -152.4 22.8

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): No Remote Control (TT C) Location(s): S14a: Street Address: Estação Terrena de Guaratiba (Primary Control Station) S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Rio de Janeiro RJ 23020-715 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 5521 2121 4440 Remote Control (TT C) Location(s): S14a: Street Address: Estação Terrena de Tanguá (Backup Control Station) S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Tangua RJ 24800-000 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 5521 2121 4023

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 1402 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1748 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 3150 3.38 0.87 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 525 2.35 0.87 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 17.62 5.43 0.76 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): 5452.5 5149.5 5452.5 5149.5 Bus (Watts): (b): (g): (l): (q): 417.6 369.5 430.4 330.6 Total (Watts): (c): (h): (m): (r): 5870.1 5519 5882.9 5480.1 Solar Array (Watts): (d): (i): (n): (s): 7409 6569.8 6874.8 6296.5 Depth of Battery (e) (j) (o) (t) Discharge (%): 75 % % 75 % % 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: 2011-09-19 08:51:23
Document Modified: 2011-09-19 08:51:23
© 2024 FCC.report
This site is not affiliated with or endorsed by the FCC