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  • 1
    Publication Date: 2018-06-08
    Description: The Mars Rover has been built, environmentally tested and qualified for the 1996 launch of the Pathfinder mission to Mars. The basic structure for the thermal control for the Mars Rover is the Warm Electronics Box (WEB). This consists of a thermal isolating composite structure with co-cured thermal control surfaces and an ultralightweight hydrophobic solid silica aerogel which minimizes conduction and radiation.
    Keywords: Lunar and Planetary Science and Exploration
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  • 2
    Publication Date: 2018-06-08
    Description: The MGS mission is one of the first major palnetary missions conducted under the new NASA Faster, Better, Cheaper guidelines. This paper provides an overview of the array design and performance, the high temperature capable design and development.
    Keywords: Lunar and Planetary Science and Exploration
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  • 3
    Publication Date: 2018-06-08
    Keywords: Lunar and Planetary Science and Exploration
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  • 4
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    Publication Date: 2018-06-08
    Description: On July 4, 1997 the Pathfinder Mission Successfully began a new era of robotic exploration of Mars. The primary scientific payload of the Pathfinder Lander is the Sojourner Truth Mars Rover, an autonomous robotic vehicle, which is exploring and conducting scientific measurements on the Mars surface.
    Keywords: Lunar and Planetary Science and Exploration
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  • 5
    Publication Date: 2019-07-13
    Description: Future extended lunar surface missions will require extensive recovery of resources to reduce mission costs and enable self-sufficiency. Water is of particular importance due to its potential use for human consumption and hygiene, general cleaning, clothes washing, radiation shielding, cooling for extravehicular activity suits, and oxygen and hydrogen production. Various water sources are inherently present or are generated in lunar surface missions, and subject to recovery. They include: initial water stores, water contained in food, human and other solid wastes, wastewaters and associated brines, ISRU water, and scavenging from residual propellant in landers. This paper presents the results of an analysis of the contribution of water recovery from life support wastes on the overall water balance for lunar surface missions. Water in human wastes, metabolic activity and survival needs are well characterized and dependable figures are available. A detailed life support waste model was developed that summarizes the composition of life support wastes and their water content. Waste processing technologies were reviewed for their potential to recover that water. The recoverable water in waste is a significant contribution to the overall water balance. The value of this contribution is discussed in the context of the other major sources and loses of water. Combined with other analyses these results provide guidance for research and technology development and down-selection.
    Keywords: Lunar and Planetary Science and Exploration
    Type: ARC-E-DAA-TN1264 , ARC-E-DAA-TN1855 , 40th International Conference on Environmental Systems; Jul 11, 2010 - Jul 15, 2010; Barcelona, Spain; Spain
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