Attachment Sched S Tech Report. SAT-PPL-20140702-00082

Attachment Sched S Tech Report.

This document pretains to SAT-PPL-20140702-00082 for Permitted List on a Satellite Space Stations filing.

IBFS_SATPPL2014070200082_1053198

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-1 7/31/2004 N

b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis:
1/2/2002 16.8 Years

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
5/31/2004 16 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:
1/6/2004 6/30/2004 648 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)
14.0 G 14.5 G R Fixed Satellite Service
11.7 G 12.2 G T Fixed Satellite Service
13.75 G 14.0 G R 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:
55.5 W The satellite network AMAZONAS-1 has been
Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be relocated from 36ºW to 55.5ºW. Under this application
N/S Station-Keeping provided (Optional): we are seeking authority to provide service with
d. Toward West: Degrees E/W
0.05 Degrees Tolerance:
AMAZONAS-1 to the U.S. territories in the Ku band.
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 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)

1 S vupku_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) 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)
KUR R 31 23 0.05 0.05 30 N 01 428 4.7 -94 20 1
KUR R 31 23 0.05 0.05 30 N 90 1 428 4.7 -94 20 1
KUT T 29.9 21.9 0.05 0.05 30 N 01 1.9 18.1 48
KUTV T 29.9 21.9 0.05 0.05 30 N 90 1 1.9 18.1 48

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 -55.5 vupkunach.gxt
KUR R X -55.5 VUPKUNAXH.gxt
KUT T C -55.5 vdwkunach.gxt -132.5 -132.5 -132.5 -132.5 -132.5
KUT T X -55.5 VDWKUNAXH.gxt
KUR R C -55.5 vupkunacv.gxt
KUR R X -55.5 VUPKUNAXV.gxt
KUTV T C -55.5 vdwkunacv.gxt -132.5 -132.5 -132.5 -132.5 -132.5
KUTV T X -55.5 VDWKUNAXV.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 (T ID Gain (dB) No. ID No.
or C)

KT1 54000 T 11738 V C 1 127.1 KR1 KURH KT1 KUTV
KT2 54000 T 11799 V C 2 127.1 KR2 KURH KT2 KUTV
KT3 54000 T 11738 H C 3 127.1 KR3 KURV KT3 KUTH
KT4 54000 T 11799 H C 4 127.1 KR4 KURV KT4 KUTH
KT5 36000 T 11972 V C 5 127.1 KR5 KURH KT5 KUTV
KT6 36000 T 12012 V C 6 127.1 KR6 KURH KT6 KUTV
KT7 36000 T 12052 V C 7 127.1 KR7 KURH KT7 KUTV
KT8 36000 T 12092 V C 8 127.1 KR8 KURH KT8 KUTV
KT9 36000 T 12132 V C 9 127.1 KR9 KURH KT9 KUTV
KT10 36000 T 12172 V C 10 127.1 KR10 KURH KT10 KUTV
KT11 36000 T 11972 H C 11 127.1 KR11 KURV KT11 KUTH
KT12 36000 T 12012 H C 12 127.1 KR12 KURV KT12 KUTH
KT13 36000 T 12052 H C 13 127.1 KR13 KURV KT13 KUTH
KT14 36000 T 12092 H C 14 127.1 KR14 KURV KT14 KUTH
KT15 36000 T 12132 H C 15 127.1 KR15 KURV KT15 KUTH
KT16 36000 T 12172 H C 16 127.1 KR16 KURV KT16 KUTH
KR1 54000 R 14034 H C
KR2 54000 R 14095 H C
KR3 54000 R 14034 V C
KR4 54000 R 14095 V C
KR5 36000 R 13772 H C
KR6 36000 R 13812 H C
KR7 36000 R 13852 H C
KR8 36000 R 13892 H C
KR9 36000 R 13932 H C
KR10 36000 R 13972 H C
KR11 36000 R 13772 V C
KR12 36000 R 13812 V C
KR13 36000 R 13852 V C
KR14 36000 R 13892 V C

KR15 36000 R 13932 V C
KR16 36000 R 13972 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 36M0G7W 36000 4 38010 0.75 6.1 18.3
3 9M00G7W 9000 8 11300 0.66666667 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. 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)
1 16 1 18 Link_Budget_1. 53 2.5 9.5 27.1 32.1 -132.5 30
1 4 4 2340 Link_Budget_2. 43 -15 -8 2.6 5.6 -137.8 31
5 16 4 2340 Link_Budget_2. 43 -15 -8 2.6 5.6 -137.8 31
1 4 4 2340 Link_Budget_3. 49.2 -16.4 -9.4 5.4 10.4 -133 26.3
5 16 4 2340 Link_Budget_3. 49.2 -16.4 -9.4 5.4 10.4 -133 26.3
1 16 2 1 Link_Budget_4. 53 16 23 40.1 45.1 -132.5 26.3
1 16 3 4 Link_Budget_5. 53 8.1 15.1 32.7 37.7 -134 30

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:
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

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:

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
2121 (meters) End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
2415
S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload:
4536 36.1 0.77
S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus:
885 7.89 0.87
S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total:
55.6 6.74 0.67

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):
7315 7315 7315 7315
Bus (Watts): (b): (g): (l): (q):
1660 940 1660 940
Total (Watts): (c): (h): (m): (r):
8975 8255 8975 8255
Solar Array (Watts): (d): (i): (n): (s):
11504 10359 9770 8906
Depth of Battery (e) (j) (o) (t)
Discharge (%):
60 % % 60 % %

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: 2014-07-03 16:37:17
Document Modified: 2014-07-03 16:37:17

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