An Environmental Control and Life Support System Concept for a Pressurized Lunar Rover
Author(s) -
Robert M. Bagdigian,
Imelda Stambaugh
Publication year - 2010
Publication title -
40th international conference on environmental systems
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2010-6256
Subject(s) - astrobiology , life support system , control (management) , computer science , environmental science , aeronautics , systems engineering , engineering , aerospace engineering , artificial intelligence , physics
Pressurized rovers can add many attractive capabilities to a human lunar exploration campaign, most notably by extending the reach of astronauts far beyond the immediate vicinities of lunar landers and fixed assets such as habitats. Effective campaigns will depend on an efficient allocation of environmental control and life support system (ECLSS) equipment amongst mobile rovers and fixed habitats such that widespread and sustainable exploration can be achieved. This paper will describe some of the key drivers that influence the design of an ECLSS for a pressurized lunar rover and a conceptual design that has been formulated to address those drivers. Opportunities to realize programmatic and operational efficiencies through commonality of rover ECLSS and extravehicular activity (EVA) equipment have also been explored and will be described. Plans for the inclusion of ECLSS functionality in prototype lunar rovers will be summarized
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