Sea Launch User's Guide

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5-11 Typical Electromagnetic Environment in Payload Processing Facility⎯ Encapsulation Cell .......................................................................................... 5-12 5-12 Typical Measured Electromagnetic Environment at the Sea Launch Home Port Pier................................................................................................ 5-13 5-13 In-Flight Electromagnetic Environment ......................................................... 5-14 5-14 Sea Launch RF Environment.......................................................................... 5-16 5-15 Payload Unit Air Conditioning Venting Scheme............................................ 5-18 5-16 Maximum Internal PLF Surface Temperatures .............................................. 5-21 5-17 Free Molecular Heating Environments........................................................... 5-22 5-18 Payload Unit Ascent Venting Scheme............................................................ 5-23 5-19 Payload Fairing Internal Pressure During Ascent........................................... 5-24 5-20 Typical Peak Ascent Depressurization ........................................................... 5-24 6-1 Zenit-3SL Coordinate System........................................................................... 6-2 6-2 Expected Spacecraft Mass and CG Limits With SCA1194 Spacecraft Adapter............................................................................................ 6-6 6-3 Expected Spacecraft Mass and CG Limits With SCA1666 Spacecraft Adapter............................................................................................ 6-7 6-4 Expected Spacecraft Mass and CG Limits With SCA702 and SCA702GEM Spacecraft Adapters................................................................... 6-8 6-5 Maximum Spacecraft Intentional Electrical Field Radiation Impingement on LV.......................................................................................... 6-9 6-6 Lightning and Weather Services Used to Determine or Forecast Lightning During Launch Campaign.............................................................. 6-10 6-7 Electrical and Mechanical Mates .................................................................... 6-14 7-1 Spacecraft Static Envelope ............................................................................... 7-1 7-2 Payload Fairing Locations for Access Doors.................................................... 7-3 7-3 SCA1666 Spacecraft Adapter........................................................................... 7-4 7-4 SCA702 Spacecraft Adapter............................................................................. 7-5 7-5 SCA1194 Spacecraft Adapter........................................................................... 7-6 7-6 Umbilical and RF Configurations During Launch Processing Flow................ 7-8 7-7 Sea Launch External Communications Network.............................................. 7-9 8-1 Spacecraft Processing Flow .............................................................................. 8-1 8-2 Nominal 60-Day Processing Schedule.............................................................. 8-2 8-3 Campaign Timeline........................................................................................... 8-3 8-4 Payload Processing Facility at Home Port........................................................ 8-4 8-5 Fit Check on Adapter Support Stand ................................................................ 8-5 8-6 SBA Vertical Mating Position .......................................................................... 8-6 8-7 SBA Horizontal Raised Position....................................................................... 8-7 8-8 SBA Rotating to Horizontal With Pathfinder Structure ................................... 8-7 8-9 EPTME With Encapsulated DemoSat Spacecraft ............................................ 8-8 8-10 Scaffolding Around Encapsulated Spacecraft .................................................. 8-9 8-11 Access to Encapsulated Spacecraft................................................................... 8-9 8-12 Payload Unit Exiting the Payload Processing Facility ................................... 8-10 8-13 Payload Unit in Transit to the Assembly and Command Ship ....................... 8-11 8-14 Payload Unit on Stern Ramp of the Assembly and Command Ship............... 8-11 8-15 Zenit-3SL Launch Vehicles in the Assembly and Command Ship ................ 8-13 xvi D688-10009-1 REV B
8-16 Payload Unit Mating to the Zenit-3SL............................................................ 8-14 8-17 Integrated Launch Vehicle Ready for Lifting................................................. 8-15 8-18 Lifting of Integrated Launch Vehicle ............................................................. 8-16 8-19 Assembly and Command Ship Departing Home Port .................................... 8-17 8-20 Launch Platform Sailing for the Equator........................................................ 8-17 8-21 Zenit-3SL Transporter/Erector........................................................................ 8-18 8-22 Launch Operations at the Launch Site............................................................ 8-20 8-23 Assembly and Command Ship and Launch Platform Connected by Link Bridge ..................................................................................................... 8-21 8-24 Liftoff From the Launch Platform .................................................................. 8-23 8-25 Launch Control Center on the Assembly and Command Ship....................... 8-24 9-1 Sea Launch Home Port Complex...................................................................... 9-2 9-2 Sea Launch Vessels........................................................................................... 9-3 9-3 Home Port Location and Vicinity..................................................................... 9-4 9-4 Payload Processing Facility⎯Interior and Exterior Views.............................. 9-6 9-5 Building 3, U.S. Sea Launch Office Facility .................................................... 9-9 9-6 Assembly and Command Ship........................................................................ 9-11 9-7 Launch Vehicle Processing⎯Main Deck....................................................... 9-11 9-8 Launch Vehicle Transfer From Assembly and Command Ship to Launch Platform in the Home Port............................................................. 9-12 9-9 Launch Vehicle Control Center⎯Shelter Deck ............................................. 9-13 9-10 Assembly and Command Ship Launch Control Center.................................. 9-13 9-11 View of Launch Control Center Consoles and Front Wall (Boeing/Customer Side of Room) .................................................................. 9-14 9-12 Spacecraft Contractor Work Area on First Bridge Deck ................................ 9-15 9-13 Assembly and Command Ship INMARSAT B .............................................. 9-16 9-14 Spacecraft Customer Accommodations.......................................................... 9-17 9-15 Assembly and Command Ship Cabin Accommodations................................ 9-18 9-16 Main Cafeteria ................................................................................................ 9-19 9-17 Assembly and Command Ship Facilities ........................................................ 9-20 9-18 Launch Platform During Final Countdown .................................................... 9-22 9-19 Spacecraft Contractor Work Areas on Launch Platform, 38500 Deck Level...................................................................................................... 9-23 10-1 ACS INTELSAT Earth Terminal ................................................................... 10-2 10-2 ACS Weather Office....................................................................................... 10-3 10-3 On-Site Meteorological Buoy......................................................................... 10-3 10-4 Sea Launch Bell 230 Helicopter ..................................................................... 10-4 10-5 Optical Tracker ............................................................................................... 10-5 10-6 Assembly and Command Ship Proton Tracking Antenna .............................. 10-6 10-7 S-Band System Radome ................................................................................. 10-7 11-1 Sea Launch Safety Integration Process........................................................... 11-2 12-1 Anomaly Resolution System........................................................................... 12-2 REV B D688-10009-1 xvii
Page 1 and 2: SM® User’s Guide _______________
Page 3 and 4: TABLE OF CONTENTS 1. INTRODUCTION .
Page 5 and 6: Mission manager and team ..........
Page 7 and 8: 6.2 Modal Frequencies..............
Page 9 and 10: Weather conditions ................
Page 11 and 12: 11.2 Safety Assessment Phases......
Page 13: LIST OF FIGURES Page 1-1 Generic In
Page 17 and 18: ABBREVIATIONS AND ACRONYMS ACS ARS
Page 19 and 20: 1. INTRODUCTION Purpose The purpose
Page 21 and 22: Milestones • Customer kickoff •
Page 23 and 24: Sea Launch Company Sea Launch Compa
Page 25 and 26: KB Yuzhnoye/PO Yuzhmash KB Yuzhnoye
Page 27 and 28: 2. VEHICLE DESCRIPTION Overview The
Page 29 and 30: Table 2-1. Flight History Component
Page 31 and 32: RD-171 engine The RD-171 engine, wh
Page 33 and 34: Block DM-SL interface plane Liquid
Page 35 and 36: 2.3 Block DM-SL—Upper Stage Confi
Page 37 and 38: Attitude control Three-axis stabili
Page 39 and 40: Spacecraft adapter Payload structur
Page 41 and 42: Cooling air From encapsulation to l
Page 43 and 44: 3. PERFORMANCE Overview The Zenit-3
Page 45 and 46: 20 N HAWAIIAN ISLANDS North Pacific
Page 47 and 48: Flight timeline Table 3-1 lists the
Page 49 and 50: Groundtrack Figure 3-3 shows the as
Page 51 and 52: Geosynchronous transfer orbit The Z
Page 53 and 54: Circular and elliptical orbits Figu
Page 55 and 56: High-energy and escape orbits Figur
Page 57 and 58: 3.5 Spacecraft Separation Separatio
Page 59 and 60: Mid 2002 6700 Planned future growth
Page 65 and 66:
Planning Phase (Through SC Delivery
Page 67 and 68:
4.2 Mission Analysis and Operations
Page 69 and 70:
SC/SLS ICD SC ICD verification plan
Page 71 and 72:
Mission-specific documentation The
Page 73 and 74:
Operations plan The operations plan
Page 75 and 76:
5.1 Transportation and Handling at
Page 77 and 78:
Vertical Horizontal Horizontal 2658
Page 79 and 80:
Base acceleration, g 1.2 1.0 0.8 0.
Page 81 and 82:
135 130 Sound pressure levels, dB 1
Page 83 and 84:
SCA1666 The shock spectrum shown in
Page 85 and 86:
5.6 Electromagnetic Environment The
Page 87 and 88:
Radiated environment There are six
Page 89 and 90:
200 180 160 140 Electric field, dB
Page 91 and 92:
Ground processing and transportatio
Page 93 and 94:
Ground processing and transportatio
Page 95 and 96:
1200 PLF separation 1000 Block DM M
Page 97 and 98:
120 100 Legend: Predicted internal
Page 99 and 100:
Contamination control during ground
Page 101 and 102:
Spacecraft isolation The spacecraft
Page 103 and 104:
6. SPACECRAFT DESIGN CONSIDERATIONS
Page 105 and 106:
6.1 Mass and Center of Gravity (CG)
Page 107 and 108:
Table 6-2. Expected Spacecraft Mass
Page 109 and 110:
7000 6000 5000 Spacecraft mass, kg
Page 111 and 112:
■ Sea Launch RF Susceptibility 16
Page 113 and 114:
6.4 Spacecraft Design Verification
Page 115 and 116:
Static loads test A spacecraft stat
Page 117 and 118:
6.5 Horizontal Handling Processing
Page 119 and 120:
7. INTERFACES 7.1 Mechanical Interf
Page 121 and 122:
360 deg 180 deg 331 deg 180 deg 360
Page 123 and 124:
SCA702 and SCA702GEM The SCA702 has
Page 125 and 126:
7.2 Electrical Interfaces Overview
Page 127 and 128:
Radio frequency link (rerad) A dire
Page 129 and 130:
8. SPACECRAFT INTEGRATION AND LAUNC
Page 131 and 132:
Days 1 2 3 4 5 6 7 8 9 101112131415
Page 133 and 134:
Figure 8-5. Fit Check on Adapter Su
Page 135 and 136:
Payload mount assembly Flexure Inte
Page 137 and 138:
34 inches 688-95510-002 Scaffold as
Page 139 and 140:
265807J3-105 Figure 8-13. Payload U
Page 141 and 142:
8.2 Phase II⎯Mating to the LV and
Page 143 and 144:
Figure 8-17. Integrated Launch Vehi
Page 145 and 146:
8.3 Phase III⎯Transit and Launch
Page 147 and 148:
Launch rehearsals Two rehearsals ar
Page 149 and 150:
Figure 8-23. Assembly and Command S
Page 151 and 152:
Figure 8-24. Liftoff From the Launc
Page 153 and 154:
8.4 Flight Operations Range trackin
Page 155 and 156:
Postlaunch reports Sea Launch provi
Page 157 and 158:
■ Integrated LV Transfer to LP Pi
Page 159 and 160:
265807J3-015R2 Figure 9-3. Home Por
Page 161 and 162:
Encapsulation cell 15 m x 38 m (50
Page 163 and 164:
Encapsulation cell The encapsulatio
Page 165 and 166:
9.2 Assembly and Command Ship Funct
Page 167 and 168:
Spacecraft checkout accommodations
Page 169 and 170:
Capabilities Launch control center
Page 171 and 172:
Customer office areas The two offic
Page 173 and 174:
265807J3-128 Figure 9-15. Assembly
Page 175 and 176:
■ Mess Hall ■ Coffee Bar ■ Ma
Page 177 and 178:
Launch vehicle in launch position L
Page 179 and 180:
Communications and access Telephone
Page 181 and 182:
Communications Internal communicati
Page 183 and 184:
Helicopter operations Sea Launch op
Page 185 and 186:
10.2 Telemetry Assets Overview Sea
Page 187 and 188:
Tracking and data relay satellite s
Page 189 and 190:
Customer responsibilities The custo
Page 191 and 192:
Phase II⎯ development The custome
Page 193 and 194:
FAA/AST compliance All launch licen
Page 195 and 196:
12. SYSTEM RELIABILITY Overview Sea
Page 197 and 198:
APPENDIX A User Questionnaire When
Page 199 and 200:
Spacecraft Orbit Parameters SI Unit
Page 201 and 202:
Effective isotropic radiated power
Page 203 and 204:
In-flight discrete commands Number
Page 205 and 206:
Dynamic Environment Allowable accel
Page 207 and 208:
Ground Processing (continued) Stand
Page 209 and 210:
Ground Processing (continued) LP (t
Page 211 and 212:
APPENDIX B. SEA LAUNCH STANDARD OFF
Page 213 and 214:
Meetings and reviews • Customer k
Page 215 and 216:
Mission integration Analyses The fo
Page 217 and 218:
HP facilities • Processing and fu
Page 219 and 220:
ACS shared areas • Launch control
Page 221 and 222:
LP security • Card readers will c
Page 223:
Facilities • Use of additional of
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