Attachment Schedule S Tech Data SAT-AMD-20060407-00040

Attachment Schedule S Tech Data

This document pretains to SAT-AMD-20060407-00040 for Amended Filing on a Satellite Space Stations filing.

IBFS_SATAMD2006040700040_493712

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:
Intelsat Americas-9 1/2/2008 N

b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis:
1/11/2004 13 Years 0

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
10/2/2007 52 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:
1/4/2007 1/12/2007 1728 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)
5925 M 6425 M R Fixed Satellite Service
3700 M 4200 M T Fixed Satellite Service
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:
97 W Intelsat North America already holds an FCC
Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be authorization to operate a satellite at this orbital
N/S Station-Keeping provided (Optional): location. This application seks authorization for a
d. Toward West: Degrees E/W
0.05 Degrees Tolerance:
replacement satellite in that same location
g. Westernmost: 129 W
e. Toward East: 0.05 Degrees 0.05 Degrees h. Easternmost: 89 W
i. Reason for service are selection (Optional):
The Intelsat Americas-9 can replace any of the Intelsat spacecraft located within this arc in case of a catastrophic fa
ilure, except for Intelsat Americas-13 at 121W.

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 Service Area 1.gxt USA, CAN, DOM, HTI, MEX, VIR, PTR, CUB
2 S Service Area 2.gxt Region 2

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)
CTF T 28.5 22.5 0.14 0.4 30 Y 01 2.8 23.6 42.2
CRF R 29.9 24.2 0.14 0.4 30 Y 0 1 646 1.8 -92 21 1
KTF T 31.3 24.3 0.14 0.4 30 N 0 1 2.9 66.7 49.5
KRF R 33 24.6 0.14 0.4 30 N 0 1 708 4.5 -96 21 1
O R 2 1 0.14 0.4 30 N 0 2

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)
CTF T C -97 ctf_co_97R.gxt -159.8 -159.8 -159.8 -159.8 -159.8
CTF T X -97 ctf_xp_97R.gxt
KTF T C -97 ktf_co_97R.gxt -151.3 -151.3 -151.3 -151.3 -151.3
KTF T X -97 ktf_xp_97R.gxt
CRF R C -97 crf_co_97R.gxt
CRF R X -97 crf_xp_97R.gxt
KRF R C -97 krf_co_97R.gxt
KRF R X -97 krf_xp_97R.gxt
O R C -97 O.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)

CT1 36000 T 3720 V C C1 114.2 CR1 CRF CT1 CTF
CT2 36000 T 3740 H C C2 114.2 CR2 CRF CT2 CTF
CT3 36000 T 3760 V C C3 114.2 CR3 CRF CT3 CTF
CT4 36000 T 3780 H C C4 114.2 CR4 CRF CT4 CTF
CT5 36000 T 3800 V C C5 114.2 CR5 CRF CT5 CTF
CT6 36000 T 3820 H C C6 114.2 CR6 CRF CT6 CTF
CT7 36000 T 3840 V C C7 114.2 CR7 CRF CT7 CTF
CT8 36000 T 3860 H C C8 114.2 CR8 CRF CT8 CTF
CT9 36000 T 3880 V C C9 114.2 CR9 CRF CT9 CTF
CT10 36000 T 3900 H C C10 114.2 CR10 CRF CT10 CTF
CT11 36000 T 3920 V C C11 114.2 CR11 CRF CT11 CTF
CT12 36000 T 3940 H C C12 114.2 CR12 CRF CT12 CTF
CT13 36000 T 3960 V C C13 114.2 CR13 CRF CT13 CTF
CT14 36000 T 3980 H C C14 114.2 CR14 CRF CT14 CTF
CT15 36000 T 4000 V C C15 114.2 CR15 CRF CT15 CTF
CT16 36000 T 4020 H C C16 114.2 CR16 CRF CT16 CTF
CT17 36000 T 4040 V C C17 114.2 CR17 CRF CT17 CTF
CT18 36000 T 4060 H C C18 114.2 CR18 CRF CT18 CTF
CT19 36000 T 4080 V C C19 114.2 CR19 CRF CT19 CTF
CT20 36000 T 4100 H C C20 114.2 CR20 CRF CT20 CTF
CT21 36000 T 4120 V C C21 114.2 CR21 CRF CT21 CTF
CT22 36000 T 4140 H C C22 114.2 CR22 CRF CT22 CTF
CT23 36000 T 4160 V C C23 114.2 CR23 CRF CT23 CTF
CT24 36000 T 4180 H C C24 114.2 CR24 CRF CT24 CTF
KT1 54000 T 11728.5 V C K1 126.9 KR1 KRF KT1 KTF
KT2 54000 T 11735 H C K2 126.9 KR2 KRF KT2 KTF
KT3 54000 T 11789.5 V C K3 126.9 KR3 KRF KT3 KTF
KT4 54000 T 11796 H C K4 126.9 KR4 KRF KT4 KTF
KT5 27000 T 11836 V C K5 126.9 KR5 KRF KT5 KTF
KT6 27000 T 11842.5 H C K6 126.9 KR6 KRF KT6 KTF

KT7 27000 T 11867 V C K7 126.9 KR7 KRF KT7 KTF
KT8 27000 T 11873.5 H C K8 126.9 KR8 KRF KT8 KTF
KT9 27000 T 11898 V C K9 126.9 KR9 KRF KT9 KTF
KT10 27000 T 11904.5 H C K10 126.9 KR10 KRF KT10 KTF
KT11 27000 T 11929 V C K11 126.9 KR11 KRF KT11 KTF
KT12 27000 T 11935.5 H C K12 126.9 KR12 KRF KT12 KTF
KT13 27000 T 11960 V C K13 126.9 KR13 KRF KT13 KTF
KT14 27000 T 11966.5 H C K14 126.9 KR14 KRF KT14 KTF
KT15 27000 T 11991 V C K15 126.9 KR15 KRF KT15 KTF
KT16 27000 T 11997.5 H C K16 126.9 KR16 KRF KT16 KTF
KT17 27000 T 12022 V C K17 126.9 KR17 KRF KT17 KTF
KT18 27000 T 12028.5 H C K18 126.9 KR18 KRF KT18 KTF
KT19 27000 T 12053 V C K19 126.9 KR19 KRF KT19 KTF
KT20 27000 T 12059.5 H C K20 126.9 KR20 KRF KT20 KTF
KT21 27000 T 12084 V C K21 126.9 KR21 KRF KT21 KTF
KT22 27000 T 12090.5 H C K22 126.9 KR22 KRF KT22 KTF
KT23 27000 T 12115 V C K23 126.9 KR23 KRF KT23 KTF
KT24 27000 T 12121.5 H C K24 126.9 KR24 KRF KT23 KTF
KT25 27000 T 12146 V C K25 126.9 KR25 KRF KT24 KTF
KT26 27000 T 12152.5 H C K26 126.9 KR26 KRF KT26 KTF
KT27 27000 T 12177 V C K27 126.9 KR27 KRF KT27 KTF
KT28 27000 T 12183.5 H C K28 126.9 KR28 KRF KT28 KTF
TLC1 1000 R 5925.5 V T
TLC2 1000 R 6424.5 H T
TLM1 100 T 4198 V T
TLM2 100 T 4198.5 V T
TLM3 100 T 4199 V T
TLM4 100 T 4199.5 V T
TLM5 100 T 11702 H T
TLM6 100 T 12198 V T
CR1 36000 R 5945 H C
CR2 36000 R 5965 V C
CR3 36000 R 5985 H C
CR4 36000 R 6005 V C
CR5 36000 R 6025 H C
CR6 36000 R 6045 V C
CR7 36000 R 6065 H C
CR8 36000 R 6085 V C
CR9 36000 R 6105 H C

CR10 36000 R 6125 V C
CR11 36000 R 6145 H C
CR12 36000 R 6165 V C
CR13 36000 R 6185 H C
CR14 36000 R 6205 V C
CR15 36000 R 6225 H C
CR16 36000 R 6245 V C
CR17 36000 R 6265 H C
CR18 36000 R 6285 V C
CR19 36000 R 6305 H C
CR20 36000 R 6325 V C
CR21 36000 R 6345 H C
CR22 36000 R 6365 V C
CR23 36000 R 6385 H C
CR24 36000 R 6405 V C
KR1 54000 R 14028.5 H C
KR2 54000 R 14035 V C
KR3 54000 R 14089.5 H C
KR4 54000 R 14096 V C
KR5 27000 R 14136 H C
KR6 27000 R 14142.5 V C
KR7 27000 R 14167 H C
KR8 27000 R 14173.5 V C
KR9 27000 R 14198 H C
KR10 27000 R 14204.5 V C
KR11 27000 R 14229 H C
KR12 27000 R 14235.5 V C
KR13 27000 R 14260 H C
KR14 27000 R 14266.5 V C
KR15 27000 R 14291 H C
KR16 27000 R 14297.5 V C
KR17 27000 R 14322 H C
KR18 27000 R 14328.5 V C
KR19 27000 R 14353 H C
KR20 27000 R 14359.5 V C
KR21 27000 R 14384 H C
KR22 27000 R 14390.5 V C
KR23 27000 R 14415 H C
KR24 27000 R 14421.5 V C

KR25 27000 R 1446 H C
KR26 27000 R 14452.5 V C
KR27 27000 R 14477 H C
KR28 27000 R 14483.5 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 47K1G1W 47.1 8 64 0.6667 10.5 22.7
2 188KG1W 188.2 8 256 0.6667 10.5 22.7
3 753KG1W 752.9 8 1024 0.6667 10.5 22.7
4 1M13G7W 1135.3 8 1544 0.6667 10.5 22.7
5 4M64G7W 4641.2 8 6312 0.6667 10.5 22.7
6 6M21G7W 6211.8 8 8448 0.6667 10.5 22.7
7 23M6G7W 23576.5 8 32064 0.6667 10.5 22.7
8 25M3G7W 25270.6 8 34368 0.6667 10.5 22.7
9 94K1G1W 94.1 4 64 0.5 4.5 16.7
10 753KG1W 752.9 4 512 0.5 4.5 16.7
11 2M27G7W 2270.6 4 1544 0.5 4.5 16.7
12 3M65G7W 3652.9 4 2484 0.5 4.5 16.7
13 9M28G7W 9282.4 4 6312 0.5 4.5 16.7
14 12M4G7W 12423.5 4 8448 0.5 4.5 16.7

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)
1 20M0F8W 20000 TV/FM 1 NTSC 2.5 2.4 15.5 29.5
2 30M0F8W 30000 TV/FM 1 NTSC 2.5 2.4 17.2 31.2
3 1M00F9D 1000 14.3 21
4 100KF9D 100 14.3 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)
C1 C24 1 1 Link_budget_T 2000 57.8 19.9 26.5 40.9 42.2 -147.3 24.1
C1 C24 2 2 18000 Link_budget_T 2000 57.8 17.1 26.5 35.4 36.7 -152.8 26.6
C1 C24 1 480 47.1 Link_budget_C 46.8 -2.3 6.2 6.4 12.4 -159.5 26.6
C1 C24 2 120 188.2 Link_budget_C 46.8 3.7 12.2 12.2 18.4 -159.5 26.6
C1 C24 3 30 752.9 Link_budget_C 46.8 9.7 18.2 18.4 24.4 -159.5 26.6
C1 C24 4 20 1135.3 Link_budget_C 46.8 11.5 20 20.2 26.2 -159.5 26.6
C1 C24 5 5 4641.2 Link_budget_C 46.8 17.6 26.1 26.3 32.3 -159.5 26.6
C1 C24 6 4 6211.8 Link_budget_C 46.8 18.9 27.4 27.6 33.6 -159.5 26.6
C1 C24 7 1 Link_budget_C 46.8 24.7 33.2 33.4 39.4 -159.5 26.6
C1 C24 8 1 Link_budget_C 46.8 25 33.5 33.7 39.7 -159.5 26.6
C1 C24 9 240 94.1 Link_budget_C 46.8 -5.9 9.7 9.4 15.4 -159.5 20.6
C1 C24 10 30 752.9 Link_budget_C 46.8 3.1 18.7 18.4 24.4 -159.5 20.6
C1 C24 11 10 2270.6 Link_budget_C 46.8 7.9 23.5 23.2 29.2 -159.5 20.6
C1 C24 12 6 3652.9 Link_budget_C 46.8 10 25.6 25.3 31.3 -159.5 20.6
C1 C24 13 2 9282.4 Link_budget_C 46.8 14 29.6 29.3 35.3 -159.5 20.6
C1 C24 14 2 12423.5 Link_budget_C 46.8 15.3 30.9 30.6 36.6 -159.5 20.6
K1 K28 1 255 47.1 Link_budget_K 54.2 -14.9 -4.6 20.4 22.4 -149.5 20.9
K1 K28 2 64 188.2 Link_budget_K 54.2 -8.9 1.4 26.4 28.4 -149.5 20.9
K1 K28 3 16 75.9 Link_budget_K 54.2 -2.9 7.4 32.4 34.4 -149.5 20.9
K1 K28 4 11 1135.3 Link_budget_K 54.2 -1.1 9.2 34.2 36.2 -149.5 20.9
K1 K28 5 3 4641.2 Link_budget_K 54.2 5 15.3 40.3 42.3 -149.5 20.9
K1 K28 6 2 6211.8 Link_budget_K 54.2 6.3 16.6 41.6 43.6 -149.5 20.9
K1 K28 7 1 Link_budget_K 54.2 12.1 22.4 47.4 49.4 -149.5 20.9
K1 K28 8 1 Link_budget_K 54.2 12.4 22.7 47.7 49.5 -149.7 20.9
K1 K28 9 129 94.1 Link_budget_K 54.2 -18.3 -1.6 18.4 25.4 -149.5 20.9
K1 K28 10 16 752.9 Link_budget_K 54.2 -9.3 7.4 27.4 34.4 -149.5 20.9
K1 K28 11 5 2270.6 Link_budget_K 54.2 -4.5 12.2 32.2 39.2 -149.5 20.9
K1 K28 12 3 3652.9 Link_budget_K 54.2 -2.4 14.3 34.3 41.3 -149.5 20.9
K1 K28 13 1 Link_budget_K 54.2 1.6 18.3 38.3 45.3 -149.5 20.9

K1 K28 14 1 Link_budget_K 54.2 2.9 19.6 39.6 46.6 -149.5 20.9

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:
22401 Juniper lats Road
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
Nuevo Riverside CA 92567
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
909-928-3446 E040125

Remote Control (TT C) Location(s):
S14a: Street Address:
22021 COMSAT Drive
S14b. City: S14c. County: S14d. State/Country S14e. Zip Code:
Clarksburg Montgomery MD 20871
S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate):
301-428-1501 KA275

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):
2825
S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload:
4825 24.8 0.9306
S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus:
3150 15.9 0.9122
S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total:
74.5 6.4 0.8488

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):
7102 7102 7102 7102
Bus (Watts): (b): (g): (l): (q):
2329 1212 2329 1212
Total (Watts): (c): (h): (m): (r):
9431 8314 9431 8314
Solar Array (Watts): (d): (i): (n): (s):
11891 10866 10712 9789
Depth of Battery (e) (j) (o) (t)
Discharge (%):
71.6 % % 71.6 % %

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: 2006-04-11 07:26:59
Document Modified: 2006-04-11 07:26:59

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