Attachment Sched S Tech Report.

This document pretains to SES-MOD-20141022-00804 for Modification on a Satellite Earth Station filing.

IBFS_SESMOD2014102200804_1066212

 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:
  ECHOSTAR-3                                                                                                                                 N

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

c. Construction Completion Date:                                         g. Total Number of Transponders:                                  k. Total Common Carrier Transponder Bandwidth:
                                                                           32                                                                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:
                                                                           768                                           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          17.8                     G        R                         Feeder Link for Broadcasting Satellite Service in FSS
12.2                    G          12.7                     G        T                         Broadcasting Satellite Service - Video

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:
  86.4 W                                                                                                                                     The ECHOSTAR-3 satellite will operate under the UK
Longitudinal Tolerance or E/W Station-Keeping:         f. Inclination Excursion or Range of orbital are in which adequate service can be     Administration's IOMSAT-S21 ITU network, which is
                                                       N/S Station-Keeping         provided (Optional):                                      filed at 86.45 W.L. The satellite will operate at 86.4
d. Toward West:                                                                                                    Degrees       E/W
                                   0.05 Degrees        Tolerance:
                                                                                                                                             W.L. in order to avoid collision with an operational
                                                                                        g. Westernmost:
e. Toward East:                    0.05 Degrees                                                                                              satellite at 86.5 W.L.
                                                                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)

SA1                S                                                   Union of the terrirtory of Chile and the -2 dB contour of beams RXR and RXL
SA2                S                                                   Union of the territrory of Chile and the -8 dB contour of beams TXR and TXL
SA3                S                                                   Visible Earth


                                                               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)
RXR R            34.3      32.3         0.1                   30 N                          SA1                                                  716     5.75         -99           20              1
RXL    R         34.3      32.3         0.1                   30 N                          SA1                                                  716     5.75         -99           20              1
TXR    T         36.4      28.4         0.1                   30 N                          SA2                2.3          60.3      54.2
TXL    T         36.4      28.4         0.1                   30 N                          SA2                2.3          67.6      54.7
OMN    R         11.3      -0.5         0.1                   30 N                       90 SA3                                                 1000    -18.7         -80
OMN T              8.4      -0.5        0.1                   30 N                       90 SA3               13.2            0.3      3.2


                                                             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)
RXR    R      C               -86.4                              RXR.gxt
RXL    R      C               -86.4                              RXL.gxt
TXR    T      C               -86.4                              TXR.gxt
TXL    T      C               -86.4                              TXL.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)

U0001         24000 R         17324           R              C            T0001             129.7 U0001           RXR        D0001         TXR
U0003         24000 R         17353.16        R              C            T0003             129.7 U0003           RXR        D0003         TXR
U0005         24000    R      17382.32        R              C            T0005             129.7   U0005         RXR        D0005         TXR
U0007         24000    R      17411.48        R              C            T0007             129.7   U0007         RXR        D0007         TXR
U0009         24000    R      17440.64        R              C            T0009             129.7   U0009         RXR        D0009         TXR
U0011         24000    R      17469.8         R              C            T0011             129.7   U0011         RXR        D0011         TXR
U0013         24000    R      17498.96        R              C            T0013             129.7   U0013         RXR        D0013         TXR
U0015         24000    R      17528.12        R              C            T0015             129.7   U0015         RXR        D0015         TXR
U0017         24000    R      17557.28        R              C            T0017             129.7   U0017         RXR        D0017         TXR
U0019         24000    R      17586.44        R              C            T0019             129.7   U0019         RXR        D0019         TXR
U0021         24000    R      17615.6         R              C            T0021             129.7   U0021         RXR        D0021         TXR
U0023         24000    R      17644.76        R              C            T0023             129.7   U0023         RXR        D0023         TXR
U0025         24000    R      17673.92        R              C            T0025             129.7   U0025         RXR        D0025         TXR
U0027         24000    R      17703.08        R              C            T0027             129.7   U0027         RXR        D0027         TXR
U0029         24000    R      17732.24        R              C            T0029             129.7   U0029         RXR        D0029         TXR
U0031         24000    R      17761.4         R              C            T0031             129.7   U0031         RXR        D0031         TXR
U0002         24000    R      17338.58        L              C            T0002             129.7   U0002         RXL        D0002         TXL
U0004         24000    R      17367.74        L              C            T0004             129.7   U0004         RXL        D0004         TXL
U0006         24000    R      17396.9         L              C            T0006             129.7   U0006         RXL        D0006         TXL
U0008         24000    R      17426.06        L              C            T0008             129.7   U0008         RXL        D0008         TXL
U0010         24000    R      17455.22        L              C            T0010             129.7   U0010         RXL        D0010         TXL
U0012         24000    R      17484.38        L              C            T0012             129.7   U0012         RXL        D0012         TXL
U0014         24000    R      17513.54        L              C            T0014             129.7   U0014         RXL        D0014         TXL
U0016         24000    R      17542.7         L              C            T0016             129.7   U0016         RXL        D0016         TXL
U0018         24000    R      17571.86        L              C            T0018             129.7   U0018         RXL        D0018         TXL
U0020         24000    R      17601.02        L              C            T0020             129.7   U0020         RXL        D0020         TXL
U0022         24000    R      17630.18        L              C            T0022             129.7   U0022         RXL        D0022         TXL
U0024         24000    R      17659.34        L              C            T0024             129.7   U0024         RXL        D0024         TXL
U0026         24000    R      17688.5         L              C            T0026             129.7   U0026         RXL        D0026         TXL
U0028         24000    R      17717.66        L              C            T0028             129.7   U0028         RXL        D0028         TXL


U0030   24000 R     17746.82   L   C   T0030   129.7 U0030   RXL     D0030   TXL
U0032   24000   R   17775.98   L   C   T0032   129.7 U0032   RXL     D0032   TXL
D0001   24000   T   12224      R   C   CMD1          CMD1    OMNRV
D0003   24000   T   12253.16   R   C   TLM1                          TLM1    OMNTV
D0005   24000   T   12282.32   R   C   TLM2                          TLM2    OMNTV
D0007   24000   T   12311.48   R   C   TLM3                          TLM3    OMNTV
D0009   24000   T   12340.64   R   C
D0011   24000   T   12369.8    R   C
D0013   24000   T   12398.96   R   C
D0015   24000   T   12428.12   R   C
D0017   24000   T   12457.28   R   C
D0019   24000   T   12486.44   R   C
D0021   24000   T   12515.6    R   C
D0023   24000   T   12544.76   R   C
D0025   24000   T   12573.92   R   C
D0027   24000   T   12603.08   R   C
D0029   24000   T   12632.24   R   C
D0031   24000   T   12661.4    R   C
D0002   24000   T   12238.58   L   C
D0004   24000   T   12267.74   L   C
D0006   24000   T   12296.9    L   C
D0008   24000   T   12326.06   L   C
D0010   24000   T   12355.22   L   C
D0012   24000   T   12384.38   L   C
D0014   24000   T   12413.54   L   C
D0016   24000   T   12442.7    L   C
D0018   24000   T   12471.86   L   C
D0020   24000   T   12501.02   L   C
D0022   24000   T   12530.18   L   C
D0024   24000   T   12559.34   L   C
D0026   24000   T   12588.5    L   C
D0028   24000   T   12617.66   L   C
D0030   24000   T   12646.82   L   C
D0032   24000   T   12675.98   L   C
CMD1     1500   R   17301.5    V   T
TLM1     1000   T   12201      V   T
TLM2     1000   T   12203      V   T
TLM3     1000   T   12699      V   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             24M0G7W              24000                 4        27647          0.691                           5.7            12.9
D2             24M0G7W              24000                 4        30719          0.768                           6.6            18.8
D3             25M8G7W              25800                 8        41200          0.639                           7.5            19.7


                                                             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)
CMD    1M50F2D              1500                          1                                                                                                                 10         22.2
TLM    1M00G2D              1000                          1                                                                                                                  9         21.2


                                                                  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        T0032      D1                                      1               LB1.docx                             65.8            6.8        13.2      46.2         54.7                      13.2
T0001        T0032      D2                                      1               LB2.docx                             65.8           6.8         13.2      46.2         54.7                      13.2
T0001        T0032      D3                                      1               LB3.docx                             65.8           6.8         13.2      46.2         54.7                      13.2
CMD1         CMD1                      CMD                      1               CMD LB.docx                          63.8          18.8           30
TLM1         TLM3                      TLM                      1               TLM LB.docx                                                                 1.1         3.2


                                                           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:
 530 Echostar Drive
S14b. City:                                S14c. County:                                   S14d. State/Country      S14e. Zip Code:
 Cheyenne                                   Laramie                                          WY                       82007
S14f. Telephone Number:                                    S14g. Call Sign of Control Station (if appropriate):
 307-633-5460

Remote Control (TT C) Location(s):
S14a: Street Address:
 801 North Dish Drive
S14b. City:                                S14c. County:                                   S14d. State/Country      S14e. Zip Code:
 Gilbert                                    Maricopa                                         AZ                       85233
S14f. Telephone Number:                                    S14g. Call Sign of Control Station (if appropriate):
 480-558-2778


                                                                          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
 1603                                                                       (meters)                          End of Life (0.0 - 1.0)
S15b. Mass of fuel and disposables at launch (kg):
  2070
S15c. Mass of spacecraft and fuel at launch (kg):                   S15f. Length (m):                       S15i. Payload:
  3673                                                               3.16                                    0.85
S15d. Mass of fuel, in orbit, at beginning of life (kg):            S15g. Width (m):                        S15j. Bus:
  440                                                                1.82                                    0.89
S15e. Deployed Area of Solar Array (square meters):                 S15h. Height (m):                       S15k. Total:
  70.5                                                               5.8                                     0.76


            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):
                                                6811.5              6811.9              6811.5              6811.9
            Bus (Watts):                 (b):                (g):                (l):                (q):
                                                613.7               508.6               617.3               508.6
            Total (Watts):               (c):                (h):                (m):                (r):
                                                7428.8              7320.5              7428.8              7320.5
            Solar Array (Watts):         (d):                (i):                (n):                (s):
                                                8809.8              8082.4              8746                8020
            Depth of Battery             (e)                 (j)                 (o)                 (t)
            Discharge (%):
                                                75       %          75       %          79.8     %          79.8     %


S17. CERTIFICATIONS:
a. Are the power flux density limits of § 25.208 met?:                                                                                    YES   NO   X    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: 2014-10-24 13:25:33
Document Modified: 2014-10-24 13:25:33

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