NASA NTRS · 20160009636
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Davoodi, Faranak. 2014-08-04. REARM: Re-entry Hopper Space-Craft System on Mars. https://ntrs.nasa.gov/citations/20160009636
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This slide presentation reviews the mission architecture for the Titan mission. The presentation includes information on mission architecture options, probe delivery options, and Enceladus lighting.
Since the Viking missions to Mars in the 1970s, accounting for the costs associated with planetary protection implementation has not been done systematically during early project formulation phases, leading to unanticipated costs during subsequent implementation phases of flight projects. The simultaneous development of more stringent planetary protection requirements, resulting from new knowledge about the limits of life on Earth, together with current plans to conduct life-detection experiments on a number of different solar system target bodies motivates a systematic approach to integrating planetary protection requirements and mission design. A current development effort at NASA's Jet Propulsion Laboratory is aimed at integrating planetary protection requirements more fully into the early phases of mission architecture formulation and at developing tools to more rigorously predict associated cost and schedule impacts of architecture options chosen to meet planetary protection requirements.
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