Attachment Sched S Tech Report.

This document pretains to SAT-PDR-20160906-00087 for Petition for Declaratory Ruling on a Satellite Space Stations filing.

IBFS_SATPDR2016090600087_1150301

                                                                                                                                                       Approved by OMD Control Number 3060-0678
                                                                                                                                                                      Estimated Burden Hours: 80


 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-95W                                                            1/1/2021                                                           N

b. Construction Commencement Date:                                      f. Estimated Lifetime of Satellite(s):                             j. Number of transponders offered on a common carrier basis:
  3/1/2018                                                                 15                                            Years                0

c. Construction Completion Date:                                        g. Total Number of Transponders:                                   k. Total Common Carrier Transponder Bandwidth:
  9/1/2020                                                                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:
 10/1/2020                             12/1/2020                          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 opera
                              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                         Feeder Link for Broadcasting Satellite Service in FSS
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:
  95.15 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 of (l) Argument of      Active Service Arc Range (Degrees)
 Plane No.     Satellites in   Angle (degrees)      Period                                        the Ascending Node         Perigee      (m) Begin    (n) End Angle    (o) Other
                   Plane                          (Seconds)                                              (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, PTR
SWU                S                        SWRR SA.gxt                SW UPLINK
CRBRSA             S                        CRBRSA.gxt                 Caribbean CMD
CRBTSA             S                        CRBTSA.gxt                 Caribbean TLM


                                                               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)
CON T             37.1     27.1       0.15       0.12         30 N                          CONUS+             1.7           202      60.2
SWR    R            47       45       0.15       0.12         30 N                          SWU                                                  900     17.5        -104           20              1
CON    T          37.1     27.1       0.15       0.12         30 N                          CONUS+             1.7           202      60.2
SWR    R            47       45       0.15       0.12         30 N                          SWU                                                  900     17.5        -104           20              1
CRB    R            47       43       0.15       0.12         30 N                          CRBRSA                                              1128     16.5        -104           20              1


CRBT T            45.5     41.5       0.15       0.12         30 N                          CRBTSA                2         0.63      43.5


                                                               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 Gain                   Max. Power Flux Density (dBW/M2/Hz)
Beam   T/R      Cross   Ref. Orbital  Contour Description    Contour Data (GXT File)   At Angle of Arrival above horizontal (for emission with highest PFD)
  ID   Mode     Polar    Longitude   (Figure/Table/ Exhibit)                           (g) 5 Deg     (h) 10 Deg      (i) 15 Deg     (j) 20 Deg    (k) 25 Deg
              Mode ("C" (Deg. E/W)
                or" X")
CON    T      C              -110.9                               CONTL.gxt                -117.1            -117         -116.9         -116.9        -116.7
CON    T      C              -110.9                               CONTR.gxt                -117.1            -117         -116.9         -116.9        -116.7
SWR    R      C              -110.9                               SWRL.gxt
SWR    R      C              -110.9                               SWRR.gxt
CRB    R      C              -110.9                               CRBR.gxt
CRBT T        C              -110.9                                CRBT.gxt                -120.1         -120.1          -120.1         -120.1        -120.1


                                                             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              121.3 CU001           SWRR       CH001         CONTL
CH003         26000 T         17354.16        L              C            T0003              121.3 CU003           SWRR       CH003         CONTL
CH005         26000 T         17383.32        L              C            T0005              121.3 CU005           SWRR       CH005         CONTL
CH007         26000 T         17412.48        L              C            T0007              121.3 CU007           SWRR       CH007         CONTL
CH009         26000 T         17441.64        L              C            T0009              121.3 CU009           SWRR       CH009         CONTL
CH011         26000 T         17470.8         L              C            T0011              121.3 CU011           SWRR       CH011         CONTL
CH013         26000 T         17499.96        L              C            T0013              121.3 CU013           SWRR       CH013         CONTL
CH015         26000 T         17529.12        L              C            T0015              121.3 CU015           SWRR       CH015         CONTL
CH017         26000 T         17558.28        L              C            T0017              121.3 CU017           SWRR       CH017         CONTL
CH019         26000 T         17587.44        L              C            T0019              121.3 CU019           SWRR       CH019         CONTL
CH021         26000 T         17616.6         L              C            T0021              121.3 CU021           SWRR       CH021         CONTL
CH023         26000 T         17645.76        L              C            T0023              121.3 CU023           SWRR       CH023         CONTL
CH025         26000 T         17674.92        L              C            T0025              121.3 CU025           SWRR       CH025         CONTL
CH002         26000 T         17325           R              C            T0002              121.3 CU002           SWRL       CH002         CONTR
CH004         26000 T         17354.16        R              C            T0004              121.3 CU004           SWRL       CH004         CONTR
CH006         26000 T         17383.32        R              C            T0006              121.3 CU006           SWRL       CH006         CONTR
CH008         26000 T         17412.48        R              C            T0008              121.3 CU008           SWRL       CH008         CONTR
CH010         26000 T         17441.64        R              C            T0010              121.3 CU010           SWRL       CH010         CONTR
CH012         26000 T         17470.8         R              C            T0012              121.3 CU012           SWRL       CH012         CONTR
CH014         26000 T         17499.96        R              C            T0014              121.3 CU014           SWRL       CH014         CONTR
CH016         26000 T         17529.12        R              C            T0016              121.3 CU016           SWRL       CH016         CONTR
CH018         26000 T         17558.28        R              C            T0018              121.3 CU018           SWRL       CH018         CONTR
CH020         26000 T         17587.44        R              C            T0020              121.3 CU020           SWRL       CH020         CONTR
CH022         26000 T         17616.6         R              C            T0022              121.3 CU022           SWRL       CH022         CONTR
CH024         26000 T         17645.76        R              C            T0024              121.3 CU024           SWRL       CH024         CONTR
CH026         26000 T         17674.92        R              C            T0026              121.3 CU026           SWRL       CH026         CONTR
CU001         26000 R         24775           R              C            CMDA                     CMD1            SWRR
CU003         26000 R         24804.16        R              C            CMDB                     CMD2            SWRR
CU005         26000 R         24833.32        R              C            TLMA                                                TEL1          CONTR
CU007         26000 R         24862.48        R              C            TLMB                                                TEL2          CONTR


CU009   26000 R   24891.64   R   C   CMDC   CMD3   CRBR
CU011   26000 R   24920.8    R   C   CMDD   CMD4   CRBR
CU013   26000 R   24949.96   R   C   TLMC                 TEL3   CRBT
CU015   26000 R   24979.12   R   C   TLMD                 TEL4   CRBT
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
CMD3     1000 R   24753      R   T
CMD4     1000 R   24755      R   T
TEL3     1000 T   17303      R   T
TEL4     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                 8        41529         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)
TLM    1M00F9D              1000                          1                                                                                                                 10           25
CMD    1M00F9D              1000                          1                                                                                                               13.3           25


                                                                  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               Service Link.pdf                     65.2            6.2          13      53.4         60.2         -116.3        18
CMDA         CMDB                      CMD                      1               CMD SWU.pdf                          65.2            5.5        21.5
TLMA         TLMB                      TLM                      1               TLM SWU.pdf                                                               15.1         25.1         -138.3       41.2
CMDC         CMDD                      CMD                      1               CMD CRB.pdf                          65.2            5.5        21.5
TLMC         TLMD                      TLM                      1               TLM CRB.pdf                                                               33.5         43.5         -120.1       41.2


                                                           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.


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Document Created: 2016-09-07 09:46:20
Document Modified: 2016-09-07 09:46:20

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