Attachment Sched S Tech Report. SAT-LOI-20141216-00130

Attachment Sched S Tech Report.

This document pretains to SAT-LOI-20141216-00130 for Letter of Intent on a Satellite Space Stations filing.

IBFS_SATLOI2014121600130_1071805

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:
BSSNET2A-115W 1/1/2018 N

b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis:
12/1/2015 15 Years 0

c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth:
6/1/2018 26 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:
6/1/2018 12/31/2018 758 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)
17.3 G 17.7 G T Broadcasting Satellite Service - Data
17.3 G 17.7 G T Broadcasting Satellite Service - Sound
17.3 G 17.7 G T Broadcasting Satellite Service - Video
17.3 G 17.7 G T TTC
24.75 G 25.25 G R Broadcasting Satellite Service - Data
24.75 G 25.25 G R Broadcasting Satellite Service - Sound
24.75 G 25.25 G R Broadcasting Satellite Service - Video
24.75 G 25.25 G R TTC

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:
115 W Available Appendix F orbital location
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:
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 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)

CONUS+ S USA, HWA, ALS
SWUL S SW UPLINK
CMD S COMMAND STATION
TEL S TELEMETRY STATION

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)
USA T 36.3 28.3 0.15 30 N CONUS+ 1.9 260 58.5
SWU R 46.8 44.8 0.15 30 N SWUL 800 17.8 -109 25 0.5
CMD R CMD
TEL T TEL

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)
USA T C -115 CONUS 115WLA -115 -115 -115 -115 -115
SWU R C -115 ULLA.gxt
CMD R C -115 ULLA.GXT
TEL T C -115 TEL.GXT -140 -140 -140 -140 -140

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)

CH001 26000 T 17325 L C T0001 156 CU001 SWUL CH001 USA
CH003 26000 T 17354.16 L C T0003 156 CU003 SWUL CH003 USA
CH005 26000 T 17383.32 L C T0005 156 CU005 SWUL CH005 USA
CH007 26000 T 17412.48 L C T0007 156 CU007 SWUL CH007 USA
CH009 26000 T 17441.64 L C T0009 156 CU009 SWUL CH009 USA
CH011 26000 T 17470.8 L C T0011 156 CU011 SWUL CH011 USA
CH013 26000 T 17499.96 L C T0013 156 CU013 SWUL CH013 USA
CH015 26000 T 17529.12 L C T0015 156 CU015 SWUL CH015 USA
CH017 26000 T 17558.28 L C T0017 156 CU017 SWUL CH017 USA
CH019 26000 T 17587.44 L C T0019 156 CU019 SWUL CH019 USA
CH021 26000 T 17616.6 L C T0021 156 CU021 SWUL CH021 USA
CH023 26000 T 17645.76 L C T0023 156 CU023 SWUL CH023 USA
CH025 26000 T 17674.92 L C T0025 156 CU025 SWUL CH025 USA
CH002 26000 T 17325 R C T0002 156 CU002 SWUL CH002 USA
CH004 26000 T 17354.16 R C T0004 156 CU004 SWUL CH004 USA
CH006 26000 T 17383.32 R C T0006 156 CU006 SWUL CH006 USA
CH008 26000 T 17412.48 R C T0008 156 CU008 SWUL CH008 USA
CH010 26000 T 17441.64 R C T0010 156 CU010 SWUL CH010 USA
CH012 26000 T 17470.8 R C T0012 156 CU012 SWUL CH012 USA
CH014 26000 T 17499.96 R C T0014 156 CU014 SWUL CH014 USA
CH016 26000 T 17529.12 R C T0016 156 CU016 SWUL CH016 USA
CH018 26000 T 17558.28 R C T0018 156 CU018 SWUL CH018 USA
CH020 26000 T 17587.44 R C T0020 156 CU020 SWUL CH020 USA
CH022 26000 T 17616.6 R C T0022 156 CU022 SWUL CH022 USA
CH024 26000 T 17645.76 R C T0024 156 CU024 SWUL CH024 USA
CH026 26000 T 17674.92 R C T0026 156 CU026 SWUL CH026 USA
CU001 26000 R 24775 R C
CU003 26000 R 24804.16 R C
CU005 26000 R 24833.32 R C
CU007 26000 R 24862.48 R C

CU009 26000 R 24891.64 R C
CU011 26000 R 24920.8 R C
CU013 26000 R 24949.96 R C
CU015 26000 R 24979.12 R C
CU017 26000 R 25008.28 R C
CU019 26000 R 25037.44 R C
CU021 26000 R 25066.6 R C
CU023 26000 R 25095.76 R C
CU025 26000 R 25124.92 R C
CU002 26000 R 24775 L C
CU004 26000 R 24804.16 L C
CU006 26000 R 24833.32 L C
CU008 26000 R 24862.48 L C
CU010 26000 R 24891.64 L C
CU012 26000 R 24920.8 L C
CU014 26000 R 24949.96 L C
CU016 26000 R 24979.12 L C
CU018 26000 R 25008.28 L C
CU020 26000 R 25037.44 L C
CU022 26000 R 25066.6 L C
CU024 26000 R 25095.76 L C
CU026 26000 R 25124.92 L C
CMD1 1000 R 24753 R T
CMD2 1000 R 24755 R T
TEL1 1000 T 17303 R T
TEL2 1000 T 17306 R 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)

D1 26M0G7W 26000 4 27647 0.6912 0 5.7 28
D2 26M0G7W 26000 4 30719 0.768 0 6.6 28
D3 26M0G7W 26000 8 41200 0.6389 0 7.5 28

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)
T0001 T0026 D1 1 115 WL Comm 67.6 9 12 50.5 58.5 -115 19.6

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:
TBD
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
3715 (meters) End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
2542
S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload:
6260 45 0.7
S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus:
277 8.2 0.85
S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total:
80 7.3 0.6

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):
14922 14922 14922 14922
Bus (Watts): (b): (g): (l): (q):
1766 955 1766 955
Total (Watts): (c): (h): (m): (r):
16688 15877 16688 15877
Solar Array (Watts): (d): (i): (n): (s):
17944 19900 17000 17500
Depth of Battery (e) (j) (o) (t)
Discharge (%):
76.5 % 76.5 % 76.5 % 76.5 %

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: 2014-12-18 10:55:02
Document Modified: 2014-12-18 10:55:02

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