Attachment Sched S Tech Report

This document pretains to SAT-LOA-20080416-00085 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2008041600085_799340

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 16 2/28/2010 N b. Construction Commencement Date: f. Estimated Lifetime of Satellite(s): j. Number of transponders offered on a common carrier basis: 11/29/2007 15 Years c. Construction Completion Date: g. Total Number of Transponders: k. Total Common Carrier Transponder Bandwidth: 9/28/2009 24 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: 10/28/2009 12/31/2009 864 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) 13750 M 14500 M R Fixed Satellite Service 11700 M 12200 M T Fixed Satellite Service 12750 M 13250 M R Direct to Home in the Fixed Fixed Satellite Service 10700 M 10950 M T Direct to Home in the Fixed Fixed Satellite Service 10950 M 11200 M T Fixed Satellite Service 11200 M 11450 M T Direct to Home in the Fixed 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: 58.1 W Replace and/or augment existing services of the IS 9 Longitudinal Tolerance or E/W Station-Keeping: f. Inclination Excursion or Range of orbital are in which adequate service can be spacecraft 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 (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 Eastern Brazil 2 S Mexico, Central America, the Caribbean, Puerto Rico 3 S Mexico, Central America 4 S Global

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) BHU R 38.4 32.4 0.12 0.11 30 N 01 518 11.3 -108.3 25 1 BVUL R 38.4 32.4 0.12 0.11 30 N 90 1 518 11.3 -108.3 25 1 BHD T 36.9 32.9 0.12 0.11 30 N 0 1 2.8 57.5 54.5 BVDL T 36.9 32.9 0.12 0.11 30 N 90 1 2.8 57.5 54.5 MHU R 38.6 30.6 0.12 0.11 30 N 0 2 518 11.5 -108.5 25 1 MVU R 38.6 30.6 0.12 0.11 30 N 90 2 518 11.5 -108.5 25 1 MHD T 36.6 32.6 0.12 0.11 30 N 0 2 2.8 57.5 54.2 MVD T 36.6 32.6 0.12 0.11 30 N 90 2 2.8 57.5 54.2 M2D T 39.6 33.6 0.12 0.11 30 N 90 3 2.8 57.5 57.2 CMD R 20.3 17.3 0.12 0.11 30 N 0 4 2272 -13.3 -112 CMD R 20.3 17.3 0.12 0.11 30 N 90 4 2272 -13.3 -112 CMD R 3 0 0.12 0.11 N 4 5590 -34.5 -90.8 CMD R 13 6 0.12 0.11 N 4 21548 -30.3 -94.9 TLM T 21.3 18.3 0.12 0.11 N 04 4.2 0.15 13.1 TLM T 3 0 0.12 0.11 N 4 5.9 2.2 6.4 TLM T 13 6 0.12 0.11 N 4 8.9 1.1 13.4 UPC T 21 17 0.12 0.11 N 04 2.2 1.1 15.6 UPC T 21 17 0.12 0.11 N 90 4 2.2 1.1 15.6

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) BHU R C -58.1 BHUL.gxt BVUL R C -58.1 BVUL.gxt BHD T C -58.1 BHDL.gxt BVDL T C -58.1 BVDL.gxt MHU R C -58.1 MHUL.gxt MVU R C -58.1 MVUL.gxt MHD T C -58.1 MHDL.gxt MVD T C -58.1 MVDL.gxt M2D T C -58.1 M2DL.gxt CMD R C -58.1 CMDH.pdf CMD R C -58.1 CMDV.pdf CMD R C -58.1 CMDO.pdf CMD R C -58.1 CMDW.pdf TLM T C -58.1 TLMH.pdf TLM T C -58.1 TLMO.pdf TLM T C -58.1 TLMW.pdf UPC T C -58.1 UPCH.gxt UPC T C -58.1 UPCV.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) BU1 36000 R 12772 H C B1 131.5 BU1 BHUL BD1 BVDL BU2 36000 R 12812 H C B2 131.5 BU2 BHUL BD2 BVDL BU3 36000 R 12852 H C B3 131.5 BU3 BHUL BD3 BVDL BU5 36000 R 12932 H C B5 131.5 BU5 BHUL BD5 BVDL BU7 36000 R 13022 H C B7 131.5 BU7 BHUL BD7 BVDL BU9 36000 R 13102 H C B9 131.5 BU9 BHUL BD9 BVDL BU10 36000 R 13142 H C B10 131.5 BU10 BHUL BD10 BVDL BU11 36000 R 13182 H C B11 131.5 BU11 BHUL BD11 BVDL BU13 36000 R 12772 V C B13 131.5 BU13 BVUL BD13 BHDL BU15 36000 R 12852 V C B15 131.5 BU15 BVUL BD15 BHDL BU16 36000 R 12892 V C B17 131.5 BU17 BVUL BD17 BHDL BU17 36000 R 12932 V C B19 131.5 BU19 BVUL BD19 BHDL BU19 36000 R 13022 V C B20 131.5 BU20 BVUL BD20 BHDL BU20 36000 R 13062 V C B21 131.5 BU21 BVUL BD21 BHDL BU21 36000 R 13102 V C B23 131.5 BU23 BVUL BD23 BHDL BU23 36000 R 13182 V C B25 131.5 BU25 BHUL BD25 BVDL BU25 36000 R 13774 H C B26 131.5 BU26 BHUL BD26 BVDL BU26 36000 R 13814 H C B27 131.5 BU27 BHUL BD26 BVDL BU27 36000 R 13854 H C B29 131.5 BU29 BHUL BD29 BVDL BU29 36000 R 13934 H C B31 131.5 BU31 BVUL BD31 BHDL BU31 36000 R 13774 V C B33 131.5 BU33 BVUL BD33 BHDL BU33 36000 R 13854 V C B34 131.5 BU34 BVUL BD34 BHDL BU34 36000 R 13894 V C B35 131.5 BU35 BVUL BD35 BHDL BU35 36000 R 13934 V C M0001 132 MU001 MVUL MD001 MHDL BD1 36000 T 10722 V C M0003 132 MU003 MVUL MD003 MHDL BD2 36000 T 10762 V C M0005 132 MU005 MVUL MD005 MHDL BD3 36000 T 10802 V C M0007 132 MU007 MVUL MD007 MHDL BD5 36000 T 10882 V C M0009 132 MU009 MVUL MD009 MHDL BD7 36000 T 11222 V C M0011 132 MU011 MVUL MD011 MHDL BD9 36000 T 11302 V C M0013 132 MU013 MVUL MD013 MHDL

BD10 36000 T 11342 V C M0015 132 MU015 MVUL MD015 MHDL BD11 36000 T 11382 V C M0017 132 MU017 MVUL MD017 MHDL BD13 36000 T 10722 H C M0019 132 MU019 MVUL MD019 MHDL BD15 36000 T 10802 H C M0021 132 MU021 MVUL MD021 MHDL BD16 36000 T 10842 H C M0023 132 MU023 MVUL MD023 MHDL BD17 36000 T 10882 H C M0002 132 MU002 MHUL MD002 MVDL BD19 36000 T 11222 H C M0004 132 MU004 MHUL MD004 MVDL BD20 36000 T 11262 H C M0006 132 MU006 MHUL MD006 MVDL BD21 36000 T 11302 H C M0008 132 MU008 MHUL MD008 MVDL BD23 36000 T 11382 H C M0010 132 MU010 MHUL MD010 MVDL BD25 36000 T 10970 V C M0012 132 MU012 MHUL MD012 MVDL BD26 36000 T 11010 V C M0014 132 MU014 MHUL MD014 MVDL BD27 36000 T 11050 V C M0016 132 MU016 MHUL MD016 MVDL BD29 36000 T 11130 V C M0018 132 MU018 MHUL MD018 MVDL BD31 36000 T 10970 H C M0020 132 MU020 MHUL MD020 MVDL BD33 36000 T 11050 H C M0022 132 MU022 MHUL MD022 MVDL BD34 36000 T 11090 H C M0024 132 MU024 MHUL MD024 MVDL BD35 36000 T 11130 H C ME001 132 EU001 MVUL MD001 MHDL EU001 36000 R 13770 V C ME003 132 EU003 MVUL MD003 MHDL EU003 36000 R 13810 V C ME005 132 EU005 MVUL MD005 MHDL EU005 36000 R 13850 V C ME007 132 EU007 MVUL MD007 MHDL EU007 36000 R 13890 V C ME009 132 EU009 MVUL MD009 MHDL EU009 36000 R 13930 V C ME011 132 EU011 MVUL MD011 MHDL EU011 36000 R 13970 V C MH002 132 MU002 MHUL MD002 M2DL MU001 36000 R 14020 V C MH004 132 MU004 MHUL MD004 M2DL MU003 36000 R 14060 V C MH006 132 MU006 MHUL MD006 M2DL MU005 36000 R 14100 V C MH008 132 MU008 MHUL MD008 M2DL MU007 36000 R 14140 V C MH010 132 MU010 MHUL MD010 M2DL MU009 36000 R 14180 V C MH012 132 MU012 MHUL MD012 M2DL MU011 36000 R 14220 V C B16 131.5 BU16 BVUL BD16 BHDL MU013 36000 R 14260 V C MU015 36000 R 14300 V C MU017 36000 R 14340 V C MU019 36000 R 14380 V C MU021 36000 R 14420 V C MU023 36000 R 14460 V C MU002 36000 R 14040 H C MU004 36000 R 14080 H C MU006 36000 R 14120 H C

MU008 36000 R 14160 H C MU010 36000 R 14200 H C MU012 36000 R 14240 H C MU014 36000 R 14280 H C MU016 36000 R 14320 H C MU018 36000 R 14360 H C MU020 36000 R 14400 H C MU022 36000 R 14440 H C MU024 36000 R 14480 H C MD001 36000 T 11720 H C MD003 36000 T 11760 H C MD005 36000 T 11800 H C MD007 36000 T 11840 H C MD009 36000 T 11880 H C MD011 36000 T 11920 H C MD013 36000 T 11960 H C MD015 36000 T 12000 H C MD017 36000 T 12040 H C MD019 36000 T 12080 H C MD021 36000 T 12120 H C MD023 36000 T 12160 H C MD002 36000 T 11740 V C MD004 36000 T 11780 V C MD006 36000 T 11820 V C MD008 36000 T 11860 V C MD010 36000 T 11900 V C MD012 36000 T 11940 V C MD014 36000 T 11980 V C MD016 36000 T 12020 V C MD018 36000 T 12060 V C MD020 36000 T 12100 V C MD022 36000 T 12140 V C MD024 36000 T 12180 V C CMD1 1000 R 13997.5 H T CMD2 1000 R 14499.5 V T CMD3 1000 R 13997.5 L T CMD4 1000 R 14499.5 L T CMD5 1000 R 13997.5 L T CMD6 1000 R 14499.5 L T

TLM1 500 T 12198.25 H T TLM2 500 T 12198.75 H T TLM3 500 T 12198.25 R T TLM4 500 T 12198.75 R T TLM5 500 T 12198.25 R T TLM6 500 T 12198.75 R T UPC1 25 T 11701.25 V T UPC2 25 T 12199.75 H T

FEDERAL COMMUNICATIONS COMMISSION Page 7: Digital Modulation SATELLITE SPACE STATION AUTHORIZATIONS FCC Form 312 - Schedule S: (Technical and Operational Description) S11. DIGITAL MODULATION PARAMETERS For each digital emission provide: (a) Digital (b) Emission (c) Assigned (d) No. of (e)Uncoded (f) FEC Error (g) CDMA (h) Total C/N (i) Single Entry Mod. ID Designator Bandwidth Phases Data Rate Correction Processing Performance C/I Objective (kHz) (kbps) Coding Rate Gain (dB) Objective (dB) (dB) D1 36M0G7W 30133 4 36863 0.75 6.1 18.5 D2 10M3G7W 6771.1 4 6000 0.5 3.9 19.1 D3 100KG7W 75.4 4 64 0.5 3 18.1 D4 1M45G7W 1229 2 512 0.5 3.4 17.9 D5 400KG7W 307 2 128 0.5 3.4 18.3

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) A1 36M0F3F 36000 TV/FM 1 NTSC 12.8 2.6 10 20

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) M0001 M0024 A1 1 IS16_SCHEDU 4000 56.9 7.4 15.4 39 43 -149.1 38 M0001 M0024 D1 1 IS16_SCHEDU 56.9 9.2 17.2 40.8 44.8 -156.1 26.7 M0001 M0024 D2 3 10300 IS16_SCHEDU 56.9 0 8 34.2 38.2 -156.2 31 M0001 M0024 D3 360 100 IS16_SCHEDU 56.9 -19.6 -11.6 14.6 18.6 -156.3 28.6 M0001 M0024 D4 24 1450 IS16_SCHEDU 56.9 -7.7 0.3 26.5 30.5 -156.5 28.6 M0001 M0024 D5 90 400 IS16_SCHEDU 52.7 -10.4 -2.4 19.6 23.6 -157.4 33.1 MH002 MH012 A1 1 IS16_SCHEDU 4000 56.9 4.5 12.5 37.1 43.1 -149 38 MH002 MH012 D1 1 IS16_SCHEDU 56.9 6.2 14.2 38.8 44.8 -156.1 31 MH002 MH012 D2 3 10300 IS16_SCHEDU 56.9 -3.2 4.8 32 38 -156.4 31 MH002 MH012 D3 360 100 IS16_SCHEDU 56.9 -20 -14.6 12.6 18.6 -156.3 28.6 MH002 MH012 D4 24 1450 IS16_SCHEDU 56.9 -10.6 -2.6 24.6 30.6 -156.4 28.6 MH002 MH012 D5 90 400 IS16_SCHEDU 52.7 -14.1 -6.1 16.9 22.9 -158.1 33.1 ME001 ME011 A1 1 IS16_SCHEDU 4000 56.9 7.4 15.4 39 43 -149.1 38 ME001 ME011 D1 1 IS16_SCHEDU 56.9 9.2 17.2 40.8 44.8 -156.1 26.7 ME001 ME011 D2 3 10300 IS16_SCHEDU 56.9 0 8 34.2 38.2 -156.2 31 ME001 ME011 D3 360 100 IS16_SCHEDU 56.9 -19.6 -11.6 14.6 18.6 -156.3 28.6 ME001 ME011 D4 24 1450 IS16_SCHEDU 56.9 -7.7 0.3 26.5 30.5 -156.5 28.6 ME001 ME011 D5 90 400 IS16_SCHEDU 52.7 -10.4 -2.4 19.6 23.6 -157.4 33.1

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: 3800 International Drive, N.W. S14b. City: S14c. County: S14d. State/Country S14e. Zip Code: Washington, D.C. DC 20008 S14f. Telephone Number: S14g. Call Sign of Control Station (if appropriate): 202-944-7701

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 1238 (meters) End of Life (0.0 - 1.0) S15b. Mass of fuel and disposables at launch (kg): 1287 S15c. Mass of spacecraft and fuel at launch (kg): S15f. Length (m): S15i. Payload: 2525 22.4 0.947 S15d. Mass of fuel, in orbit, at beginning of life (kg): S15g. Width (m): S15j. Bus: 507 5.1 0.85 S15e. Deployed Area of Solar Array (square meters): S15h. Height (m): S15k. Total: 13 7.4 0.805 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): 4665 4665 4665 4665 Bus (Watts): (b): (g): (l): (q): 1389 945 1389 945 Total (Watts): (c): (h): (m): (r): 6054 5610 6054 5610 Solar Array (Watts): (d): (i): (n): (s): 6935 6221 6733 6011 Depth of Battery (e) (j) (o) (t) Discharge (%): 69.3 % % 70.1 % % 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: 2010-02-03 14:13:44
Document Modified: 2010-02-03 14:13:44
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