ESA Document - Emits - ESA

s
PROJECT
Assessment Study
Report: CDF-20(A)
February 2004
page 10 of 422
FIGURE 2-54: LAUNCH OF TMI STAGE 1......................................................................................................................97
FIGURE 2-55: LAUNCH OF ERC AND APPENDAGE........................................................................................................97
FIGURE 2-56: LAUNCH OF MEV ..................................................................................................................................98
FIGURE 2-57: ASSEMBLY SCENARIO ............................................................................................................................99
FIGURE 2-58: RISK REDUCTION POTENTIAL ...............................................................................................................104
FIGURE 2-59: RISK ASSESSMENT PROCESS .................................................................................................................105
FIGURE 2-60: HMM COMMUNICATION NETWORK ....................................................................................................118
FIGURE 2-61: TRANSFER VEHICLE CUTAWAY............................................................................................................119
FIGURE 2-62: ASTRONAUT POSING VIEW ...................................................................................................................119
FIGURE 3-1: ONE-MODULE CONFIGURATION..............................................................................................................130
FIGURE 3-2: PARALLEL CONFIGURATION ...................................................................................................................131
FIGURE 3-3: CROSS CONFIGURATION .........................................................................................................................131
FIGURE 3-4: COMPLETE VEHICLE ..............................................................................................................................132
FIGURE 3-5: GLOBAL DIMENSIONS COMPLETE VEHICLE TOP VIEW (DIMENSIONS IN MM) ...........................................132
FIGURE 3-6: GLOBAL DIMENSIONS COMPLETE VEHICLE SIDE VIEW (DIMENSIONS IN MM) ..........................................133
FIGURE 3-7: MAIN CYLINDER (DIMENSIONS IN MM)...................................................................................................134
FIGURE 3-8: BACK NODE ...........................................................................................................................................134
FIGURE 3-9: FRONT NODE..........................................................................................................................................135
FIGURE 3-10: COMPLETE PROPULSION MODULE.........................................................................................................136
FIGURE 3-11: BACKBONE STRUCTURE.......................................................................................................................136
FIGURE 3-12: ALL THREE PROPULSION SYSTEMS .......................................................................................................137
FIGURE 3-13: GLOBAL DIMENSIONS OF THE PROPULSION MODULE ............................................................................137
FIGURE 3-14: CONICAL ADAPTER WITH TANKS (CONSUMABLES)...............................................................................137
FIGURE 3-15: RECOMMENDATIONS FOR VOLUMES FOR DIFFERENT AREAS OF THE PRIVATE ZONE .............................138
FIGURE 3-16: RECOMMENDATIONS FOR VOLUMES FOR DIFFERENT AREAS OF THE PERSONAL ZONE ..........................139
FIGURE 3-17: RECOMMENDATIONS FOR VOLUMES FOR DIFFERENT AREAS OF THE PERSONAL ZONE ..........................139
FIGURE 3-18: RECOMMENDATIONS FOR VOLUMES FOR DIFFERENT AREAS OF THE SOCIAL ZONE ...............................140
FIGURE 3-19: LEVELS..................................................................................................................................................144
FIGURE 3-20: ORIENTATION OPTIONS ........................................................................................................................144
FIGURE 3-21: AXONOMETRIC VIEW OF THE FINAL BASELINE DESIGN.........................................................................146
FIGURE 3-22: BASELINE DESIGN OVERVIEW - DRAWING ............................................................................................147
FIGURE 3-23: BASELINE DESIGN OVERVIEW – DRAWING OF MEASUREMENTS............................................................148
FIGURE 3-24: BASELINE DESIGN BACK NODE – DRAWING..........................................................................................149
FIGURE 3-25: BASELINE DESIGN PERSONAL AREA - DRAWING ...................................................................................150
FIGURE 3-26: BASELINE DESIGN PRIVATE ZONE – DRAWING......................................................................................151
FIGURE 3-27: BASELINE DESIGN SOCIAL ZONE - DRAWING ........................................................................................152
FIGURE 3-28: BASELINE DESIGN FRONT NODE - DRAWING .........................................................................................153
FIGURE 3-29: BASELINE DESIGN COMPLETE OVERVIEW.............................................................................................154
FIGURE 3-30: WASTE STRATEGY................................................................................................................................161
FIGURE 3-31: MARS THM LSS DESIGN.....................................................................................................................162
FIGURE 3-32: THERMAL BUS (PRIMARY AND SECONDARY LOOP)...............................................................................170
FIGURE 3-33: HABITAT MODULE / PRIMARY LOOP PRINCIPLES ...........................................................................................171
FIGURE 3-34: SECONDARY LOOP AND RADIATORS............................................................................................................175
FIGURE 3-35: COMPARATIVE MONOPHASIC / DIPHASIC......................................................................................................176
FIGURE 3-36: TOTAL ENERGY ON RADIATOR (L), RADIATOR SIZE VERSUS ANGLE AND TEMP. FLUID (R) ...................................177
FIGURE 3-37: DEBRIS SHIELDING/THERMAL PROTECTION (L), MAX. TEMP. OF EXTERNAL LAYER (NEXTEL) (R)......178
FIGURE 3-38: POWER REQUIRED TO MAINTAIN TEMPERATURE (L), COIL SYSTEM + HEAT PIPES SCHEMATIC (R).........................179
FIGURE 3-39: OVERALL VIEW OF RADIATORS (SIZE: 2 X 57M 2 ) ...........................................................................................179
FIGURE 3-40: OXYGEN TANK DIMENSIONS.................................................................................................................180
FIGURE 3-41: TES (L) AND IMAS (R) PULSE TUBES (L), CRYOSTAT AND COOLERS SCHEMATIC (R)........................181
FIGURE 3-42: TV MISSION MODES............................................................................................................................183
FIGURE 3-43: MASS BUDGET FOR MULTI-JUNCTION CELLS OPTIONS ..........................................................................186
FIGURE 3-44: POWER SYSTEM OVERALL ARCHITECTURE ...........................................................................................187
FIGURE 3-45: MASS BUDGET......................................................................................................................................188
FIGURE 3-46: VEHICLE CONFIGURATION....................................................................................................................190
FIGURE 3-47: HABITATION MODULE ACS..................................................................................................................190