Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20080929-00203 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2008092900203_439176

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-21 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: 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: 960 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) 14.00 G 14.50 G R Fixed Satellite Service 11.70 G 12.20 G T Fixed Satellite Service 14.00 G 14.50 G R Direct to Home in the Fixed Fixed Satellite Service 11.70 G 12.20 G T 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: 125 W Orbital location is available for licensing, and is Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be suitable for providing coverage to all the 50 states. 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) NA-UL E North America, G/T contours: -5.5 dB/K contour NA-DL E North America, EIRP contours: 40 dBW contour

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) KRV R 33 23 0.15 0 30 Y 90 NA-UL 708 4.5 -97.5 21 1 KRH R 33 23 0.15 0 30 Y 0 NA-UL 708 4.5 -97.5 21 1 KTV T 34 24 0.15 0 30 Y 90 NA-DL 2.5 40 50 KTH T 34 24 0.15 0 30 Y 0 NA-DL 2.5 40 50

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) KRV R C -125 amc21_gain_UL KRH R C -125 amc21_gain_UL KTV T C -125 amc21_gain_DL -153.8 -153.3 -152.3 -151.8 -151.3 KTH T C -125 amc21_gain_DL -153.8 -153.3 -152.3 -151.8 -151.3

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) KR001 36000 R 14020 V C K0004 128 KR004 KRH KT004 KTV KR002 36000 R 14040 H C K0006 128 KR006 KRH KT006 KTV KR003 36000 R 14060 V C K0008 128 KR008 KRH KT008 KTV KR004 36000 R 14080 H C K0010 128 KR010 KRH KT010 KTV KR005 36000 R 14100 V C K0012 128 KR012 KRH KT012 KTV KR006 36000 R 14120 H C K0001 128 KR001 KRV KT001 KTH KR007 36000 R 14140 V C K0003 128 KR003 KRV KT003 KTH KR008 36000 R 14160 H C K0005 128 KR005 KRV KT005 KTH KR009 36000 R 14180 V C K0007 128 KR007 KRV KT007 KTH KR010 36000 R 14200 H C K0009 128 KR009 KRV KT009 KTH KR011 36000 R 14220 V C K0011 128 KR011 KRV KT011 KTH KR012 36000 R 14240 H C K0013 128 KR013 KRV KT013 KTH KR013 36000 R 14260 V C K0015 128 KR015 KRV KT015 KTH KR014 36000 R 14280 H C K0017 128 KR017 KRV KT017 KTH KR015 36000 R 14300 V C K0019 128 KR019 KRV KT019 KTH KR016 36000 R 14320 H C K0021 128 KR021 KRV KT021 KTH KR017 36000 R 14340 V C K0002 128 KR002 KRH KT002 KTV KR018 36000 R 14360 H C K0014 128 KR014 KRH KT014 KTV KR019 36000 R 14380 V C K0016 128 KR016 KRH KT016 KTV KR020 36000 R 14400 H C K0018 128 KR018 KRH KT018 KTV KR021 36000 R 14420 V C K0020 128 KR020 KRH KT020 KTV KR022 36000 R 14440 H C K0022 128 KR022 KRH KT022 KTV KR023 36000 R 14460 V C K0024 128 KR024 KRH KT024 KTV KR024 36000 R 14480 H C C1 TC KRV KT001 36000 T 11720 H C T1 TM1 KTV KT002 36000 T 11740 V C T2 TM2 KTH KT003 36000 T 11760 H C C2 TCB KRH KT004 36000 T 11780 V C K0023 128 KR023 KRV KT023 KTH KT005 36000 T 11800 H C KT006 36000 T 11820 V C

KT007 36000 T 11840 H C KT008 36000 T 11860 V C KT009 36000 T 11880 H C KT010 36000 T 11900 V C KT011 36000 T 11920 H C KT012 36000 T 11940 V C KT013 36000 T 11960 H C KT014 36000 T 11980 V C KT015 36000 T 12000 H C KT016 36000 T 12020 V C KT017 36000 T 12040 H C KT018 36000 T 12060 V C KT019 36000 T 12080 H C KT020 36000 T 12100 V C KT021 36000 T 12120 H C KT022 36000 T 12140 V C KT023 36000 T 12160 H C KT024 36000 T 12180 V C TC 800 R 14001.0 V T TM1 300 T 11700.75 V T TM2 300 T 12199.25 H T TCB 800 R 14499.0 H 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 0.69 6.8 18 B 27M0G7W 27000 4 32000 0.69 6.8 18 C 6M95G1W 6950 4 8000 0.69 6.8 18 D 5M00G1W 5000 4 6000 0.69 6.8 18 E 100KG1W 100 4 56 0.69 6.8 18 F 1M60G1W 1600 4 1544 0.69 6.8 18 G 33M0G7W 33000 8 50000 0.61 9.9 20

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) H 36M0F3F 36000 TV/FM 1 NTSC 12.8 1.29 11 21 I 800KF9D 800 10 21 J 300KF9D 300 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) K0001 K0024 A 1 link_budgets.xl 57.2 20 25 46.4 49.4 -152.7 17.1 K0001 K0024 B 1 link_budgets.xl 57.2 20 25 46.4 49.4 -151.4 17.1 K0001 K0024 C 5 6950 link_budgets.xl 52.9 8.9 14 35.7 40.7 -154.2 25.6 K0001 K0024 D 6 5000 link_budgets.xl 52.9 8.9 14 34.3 39.3 -154.2 25.6 K0001 K0024 E 250 100 link_budgets.xl 46.6 -2 3 18.5 23.5 -153 19.6 K0001 K0024 F 20 1544 link_budgets.xl 46.6 8 13 28.5 33.5 -155 25.6 K0001 K0024 G 1 link_budgets.xl 47.2 20 25 46.4 49.4 -152.3 25.6 K0001 K0024 H 1 TVFM_budget.x 6000 57.2 20 26 46.4 49.4 -144.9 19.6 C1 C2 I 1 TTC_budgets.xl 59.8 10 20 T1 T1 J 1 TTC_budgets.xl 15 20 35 T2 T2 J 1 TTC_budgets.xl 15 20 35

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 Vally Spacecraft control 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

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 2000 (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: 4400 27 0.85 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 1000 5.5 0.88 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 70 3.9 0.75 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): 6200 6200 6200 6200 Bus (Watts): (b): (g): (l): (q): 540 450 620 480 Total (Watts): (c): (h): (m): (r): 6740 6650 6820 6680 Solar Array (Watts): (d): (i): (n): (s): 10400 9200 8900 7900 Depth of Battery (e) (j) (o) (t) Discharge (%): 80 % 80 % 80 % 80 % S17. CERTIFICATIONS: a. Are the power flux density limits of § 25.208 met?: YES NO X 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: 2005-06-29 12:43:04
Document Modified: 2005-06-29 12:43:04
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