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Pages 638-642

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From page 638...
... 638 ORIGINS, WORLDS, AND LIFE FIGURE C-1  Schematic illustration of the flow of the Aerospace Corporation's technical risk and cost evaluation (TRACE) process.
From page 639...
... APPENDIX C 639 The evaluation of technology, cost, and schedule are inextricably intertwined. However, it is easier to describe each element of the overall analysis (e.g., technical, schedule, and cost)
From page 640...
... 640 ORIGINS, WORLDS, AND LIFE on the information provided by the various mission study teams with a focus on treating all projects equally. To be consistent for all concepts, the TRACE cost process allows an increase in cost resulting from increased contingency mass and power, increased schedule, increased required launch vehicle capability, and other cost threats depending on the concept maturity and specific risk assessment of a particular concept.
From page 641...
... APPENDIX C 641 TRACE RESULTS FOR PRIORITY MISSIONS Summaries of the results of the TRACE evaluations of the 17 priority missions identified by the decadal survey because of their potential to address the 12 key science goals (see Chapters 4 to 15) and potential technical viability presented in Boxes C-1 through C-18.
From page 642...
... 642 ORIGINS, WORLDS, AND LIFE BOX C-1 Mercury Lander Scientific Objectives as Studied Geochemistry: Investigate the mineralogy and chemistry of Mercury's surface Geophysics: Characterize Mercury's interior structure and magnetic field Space Environment: Determine the active processes that produce Mercury's exosphere and alter its regolith Cruise Configuration Geology: Characterize the landing site at a variety of scales and provide context for landed measurements Landed Configuration Key Features Key Challenges Lander (10.5-yr life, 10-yr cruise, 0.2-yr orbital mission, 0.3-yr landed mission) Maintaining safe thermal control at close solar distance Payload: (11 instruments)

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