Attachment Schedule S Tech Data SAT-PPL-20090528-00061

Attachment Schedule S Tech Data

This document pretains to SAT-PPL-20090528-00061 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2009052800061_714194

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:
AMAZONAS-2 N

b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis:
2/16/2007 15 Years

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
36 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:
6/1/2009 11/30/2009 1500 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 G 14.5 G R Fixed Satellite Service
11.7 G 12.2 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:
61 W This position was granted by Brasilian administration.
Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be Under this application, we are only seeking authority to
N/S Station-Keeping provided (Optional): provide service to the U.S. territories in the standard
d. Toward West: Degrees E/W
0.05 Degrees Tolerance:
Ku band (14-14.5 GHz and 11.7-12.2 GHz).
g. Westernmost:
e. Toward East: 0.05 Degrees 0.07 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)

1 S AMA2_NA_SA.gxt 01

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)
KUR R 33 25 0.05 0.05 30 N 01 427 6.7 -98.7 18 1
KUR R 33 25 0.05 0.05 30 N 90 1 427 6.7 -98.7 18 1
KUT T 34.3 26.3 0.05 0.05 30 N 01 2.4 17.7 52
KUT T 34.3 26.3 0.05 0.05 30 N 90 1 2.4 17.7 52

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)
KUR R C -61 AMA2_NA_RX_H_C.gxt
KUR R X -61 AMA2_NA_RX_H_X.gxt
KUT T C -61 AMA2_NA_TX_H_C.gxt -132 -132 -132 -132 -132
KUT T X -61 AMA2_NA_TX_H_X.gxt
KUR R C -61 AMA2_NA_RX_V_C.gxt
KUR R X -61 AMA2_NA_RX_V_X.gxt
KUT T C -61 AMA2_NA_TX_V_C.gxt -132 -132 -132 -132 -132
KUT T X -61 AMA2_NA_TX_V_X.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)

KT1 36000 T 11972 V C 1 130 KR1 KURH KT1 KUTV
KT2 36000 T 12012 V C 2 130 KR2 KURH KT2 KUTV
KT3 36000 T 12052 V C 3 130 KR3 KURH KT3 KUTV
KT4 36000 T 12092 V C 4 130 KR4 KURH KT4 KUTV
KT5 36000 T 12132 V C 5 130 KR5 KURH KT5 KUTV
KT6 36000 T 12172 V C 6 130 KR6 KURH KT6 KUTV
KT7 36000 T 11972 H C 7 130 KR7 KURV KT7 KUTH
KT8 36000 T 12012 H C 8 130 KR8 KURV KT8 KUTH
KT9 36000 T 12052 H C 9 130 KR9 KURV KT9 KUTH
KT10 36000 T 12092 H C 10 130 KR10 KURV KT10 KUTH
KT11 36000 T 12132 H C 11 130 KR11 KURV KT11 KUTH
KT12 36000 T 12172 H C 12 130 KR12 KURV KT12 KUTH
KT13 36000 T 11730 V C 13 130 KR13 KURH KT13 KUTV
KT14 36000 T 11770 V C 14 130 KR14 KURH KT14 KUTV
KT15 36000 T 11810 V C 15 130 KR15 KURH KT15 KUTV
KT16 36000 T 11850 V C 16 130 KR16 KURH KT16 KUTV
KT17 36000 T 11890 V C 17 130 KR17 KURH KT17 KUTV
KT18 36000 T 11930 V C 18 130 KR18 KURH KT18 KUTV
KT19 36000 T 11730 H C 19 130 KR19 KURV KT19 KUTH
KT20 36000 T 11770 H C 20 130 KR20 KURV KT20 KUTH
KT21 36000 T 11810 H C 21 130 KR21 KURV KT21 KUTH
KT22 36000 T 11850 H C 22 130 KR22 KURV KT22 KUTH
KT23 36000 T 11890 H C 23 130 KR23 KURV KT23 KUTH
KT24 36000 T 11930 H C 24 130 KR24 KURV KT24 KUTH
KR13 36000 R 14030 H C 25 130 KR25 KURH KT25 KUTV
KR14 36000 R 14070 H C 26 130 KR26 KURH KT26 KUTV
KR15 36000 R 14110 H C 27 130 KR27 KURH KT27 KUTV
KR16 36000 R 14150 H C 28 130 KR28 KURH KT28 KUTV
KR17 36000 R 14190 H C 29 130 KR29 KURH KT29 KUTV
KR18 36000 R 14230 H C 30 130 KR30 KURH KT30 KUTV

KR19 36000 R 14030 V C 31 130 KR31 KURV KT31 KUTH
KR20 36000 R 14070 V C 32 130 KR32 KURV KT32 KUTH
KR21 36000 R 14110 V C 33 130 KR33 KURV KT33 KUTH
KR22 36000 R 14150 V C 34 130 KR34 KURV KT34 KUTH
KR23 36000 R 14190 V C 35 130 KR35 KURV KT35 KUTH
KR24 36000 R 14230 V C 36 130 KR36 KURV KT36 KUTH
KT25 36000 T 10975 V C
KT26 36000 T 11015 V C
KT27 36000 T 11055 V C
KT28 36000 T 11095 V C
KT29 36000 T 11135 V C
KT30 36000 T 11175 V C
KT31 36000 T 10975 H C
KT32 36000 T 11015 H C
KT33 36000 T 11055 H C
KT34 36000 T 11095 H C
KT35 36000 T 11135 H C
KT36 36000 T 11175 H C
KR25 36000 R 14271 H C
KR26 36000 R 14311 H C
KR27 36000 R 14351 H C
KR28 36000 R 14391 H C
KR29 36000 R 14431 H C
KR1 36000 R 13772 H C
KR2 36000 R 13812 H C
KR3 36000 R 13852 H C
KR4 36000 R 13892 H C
KR5 36000 R 13932 H C
KR6 36000 R 13972 H C
KR7 36000 R 13772 V C
KR8 36000 R 13812 V C
KR9 36000 R 13852 V C
KR10 36000 R 13892 V C
KR11 36000 R 13932 V C
KR12 36000 R 13972 V C
KR30 36000 R 14471 H C
KR31 36000 R 14271 V C
KR32 36000 R 14311 V C
KR33 36000 R 14351 V C

KR34 36000 R 14391 V C
KR35 36000 R 14431 V C
KR36 36000 R 14471 V 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)

1 1M80G7W 1800 4 2048 0.75 9 17.7
2 33M0G7W 33000 4 38010 0.75 6.1 18.3
3 7M89G7W 9000 8 11300 0.67 8 20.2
4 14K0G7W 14 4 11 0.5 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)

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)
1 36 1 18 LINK_BUDGET 53.2 1.2 9.2 30 32 -132.5 30
1 36 2 1 LINK_BUDGET 53.2 11.8 19.8 41.7 43.7 -133.5 26
1 36 3 4 LINK_BUDGET 49.4 8.1 16.1 36.6 38.6 -132.4 26.5
1 36 4 2337 LINK_BUDGET 43.4 -17.9 -9.9 3.15 5.15 -138.3 33

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:
PRAIA DO FLAMENGO 200
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
RIO DE JANEIRO BRAZIL 22210-030
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
+552198582255

Remote Control (TT C) Location(s):
S14a: Street Address:
CARRETERA M 220, KM 1,800
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
ARGANDA DEL REY SPAIN 28500
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
+34918700160

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
2505 (meters) End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
2931
S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload:
5436 28 0.91
S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus:
861 8.6 0.86
S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total:
71.41 6.7 0.78

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):
12020 12020 12020 12020
Bus (Watts): (b): (g): (l): (q):
2408 1016 2386 1011
Total (Watts): (c): (h): (m): (r):
14428 13036 14406 13031
Solar Array (Watts): (d): (i): (n): (s):
16006 14348 15380 13966
Depth of Battery (e) (j) (o) (t)
Discharge (%):
65 % % 69 % %

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: 2009-05-29 11:35:40
Document Modified: 2009-05-29 11:35:40

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