Attachment Schedule S Tech Data SAT-AMD-20040312-00033

Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20040312-00033 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2004031200033_368224

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:
GESN @15E N

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

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
0 MHz

d. Estimated Launch Date: h. Total Transponder Bandwidth (no. transponders x Bandwidth) l. Orbit Type: Mark all boxes that apply:
18000 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)
47.2 G 47.5 G R Gateway beams - 1 x 300 MHz channel
47.5 G 47.9 G R Gateway and user beams - 1 x 400 MHz channel
47.9 G 48.2 G R Gateway beams - 1 x 300 MHz channel
48.2 G 50.2 G R 4 x 500 MHz channels
37.5 G 40.0 G T Gateway/ Hub applications - 5 x 500 MHz channels
40.0 G 42.0 G T 4 x 500 MHz channels
3650 M 3700 M T Telemetry- 2 MHz spectrum of this band (TT&C)
6425 M 6525 M R Telecommand: 2 MHz spectrum of this band (TT&C)

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:
15 E Part of GESN satellite system.
Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be
N/S Station-Keeping provided (Optional):
d. Toward West: Degrees E/W
0.05 Degrees Tolerance:
g. Westernmost: 11 E
e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 19 E
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 AAB

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)
V3R T 53 50 0.05 30 Y 1 2 12.6 64
V4R T 53 50 0.05 30 Y 1 2 25.2 67
V5R R 54.4 51.4 0.05 30 Y 1 520 27.2 -95.3

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)

V1 300000 R 47350 L C
V1 300000 R 47350 R C
V2 400000 R 47700 L C
V2 400000 R 47700 R C
V3 300000 R 48050 L C
V3 300000 R 48050 R C
V4 500000 R 48450 L C
V4 500000 R 48450 R C
V5 500000 R 48950 L C
V5 500000 R 48950 R C
V6 500000 R 49450 L C
V6 500000 R 49450 R C
V7 500000 R 49950 R C
V7 500000 R 49950 L C
T2 2000 R 6435 H T
T3 2000 R 6445 H T
V1T 500000 T 37750 L C
V1T 500000 T 37750 R C
V2T 500000 T 38250 L C
V2T 500000 T 38250 R C
V3T 500000 T 38750 L C
V3T 500000 T 38750 R C
V4T 500000 T 39250 L C
V4T 500000 T 39250 R C
V5T 500000 T 39750 L C
V5T 500000 T 39750 R C
V6T 500000 T 40250 L C
V6T 500000 T 40250 R C
V7T 500000 T 40750 L C
V7T 500000 T 40750 R C

V8T 500000 T 41250 L C
V8T 500000 T 41250 R C
V9T 500000 T 41750 L C
V9T 500000 T 41750 L C
T4 2000 T 3660 H T
T4 2000 T 3670 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)

D01 491MG7W 491000 4 706000 0.9 9.3 21.3
D02 175MG7W 175000 4 252000 0.9 9.3 21.3
D03 87M8G7W 87800 4 63000 0.4 7.1 19.1
D04 35M1G7W 35100 4 25000 0.4 7.1 19.1
D05 250MG7W 250000 4 149000 0.45 4.2 16.4
D06 125MG7W 125000 4 74000 0.45 4.2 16.4
D07 500MG7W 500000 8 748000 0.75 8.6 20.8
D08 600KG7D 600 2 300 1 15 27
D09 1M00G7D 1000 2 500 1 15 27

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)

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:
TBD
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
TDB USA
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
2700 (meters) End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
2800
S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload:
5500 4.8 0.78
S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus:
1700 2.5 0.93
S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total:
38 2.5 0.72

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):
8600 8170 7050 6696
Bus (Watts): (b): (g): (l): (q):
2100 2000 1720 1639
Total (Watts): (c): (h): (m): (r):
10700 10170 8770 8335
Solar Array (Watts): (d): (i): (n): (s):
11200 10670 9180 8745
Depth of Battery (e) (j) (o) (t)
Discharge (%):
70 % 70 % 70 % 70 %

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: 2004-04-12 11:10:09
Document Modified: 2004-04-12 11:10:09

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