ESA Document - Emits - ESA

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PROJECT
Assessment Study
Report: CDF-20(A)
February 2004
page 18 of 422
TABLE 4-48: PROPULSION SYSTEM ............................................................................................................................363
TABLE 4-49: REFERENCE DATA TO CALCULATE HEAT FLUX ......................................................................................364
TABLE 4-50: MARS REFERENCE ELLIPSOID PARAMETER...........................................................................................365
TABLE 4-51: MAV ASCENT TRAJECTORY. SEQUENCE OF EVENTS .............................................................................366
TABLE 4-52: SIMULATION RESULTS ...........................................................................................................................372
TABLE 4-53: GNC EQUIPMENT CHARACTERISTICS ....................................................................................................376
TABLE 4-54: GNC EQUIPMENT: MASS BUDGET..........................................................................................................377
TABLE 4-55: MASS AND POWER BUDGETS .................................................................................................................378
TABLE 4-56: SHM STRUCTURES MASS BUDGET ........................................................................................................380
TABLE 4-57: THERMAL CASES DEFINITION ................................................................................................................384
TABLE 4-58: MAIN FEATURES....................................................................................................................................387
TABLE 4-59: OVERALL BUDGET.................................................................................................................................388
TABLE 4-60: MAV MASS BUDGET............................................................................................................................390
TABLE 4-61: POWER BUDGET- DESCENT...................................................................................................................390
TABLE 4-62: POWER BUDGET- DOCKING ..................................................................................................................390
TABLE 4-63: THERMAL CONSTRAINTS.......................................................................................................................391
TABLE 4-64: PROPULSION SYSTEM FOR THE FIRST STAGE ..........................................................................................392
TABLE 4-65: PROPULSION SYSTEM FOR THE SECOND STAGE ......................................................................................393
TABLE 4-66: MASS ESTIMATES FOR A MISSION USING CURRENT TECHNOLOGY .......................................................396
TABLE 4-67: DETAILED MASS BUDGET FOR THE ANTICIPATED LIFE SUPPORT SYSTEM ...............................................397
TABLE 4-68: MASS BUDGETS.....................................................................................................................................398
TABLE 4-69: POWER BUDGETS...................................................................................................................................398
TABLE 4-70: VOLUME REQUIREMENTS ......................................................................................................................398
TABLE 4-71: X-BAND LINK MAV-RELAY SATELLITE. ...............................................................................................399
TABLE 4-72: MAV COMMUNICATIONS BUDGET ........................................................................................................399
TABLE 6-1: COMPARISON OF BASIC REACTOR DESIGN CHOICES.................................................................................406