DocumentCode
975416
Title
First Mars outpost power systems
Author
Littman, Frank
Author_Institution
Rocketdyne Div., Rockwell Int. Corp., Canoga Park, CA, USA
Volume
8
Issue
12
fYear
1993
Firstpage
30
Lastpage
34
Abstract
Research into potential power systems for the First Mars Outpost (FMO) was performed. The author examined a representative mission architecture which was developed by NASA to determine power system requirements. Power system options including nuclear, isotope, photovoltaic (PV), chemical heat engine, and regenerative fuel cell (RFC) concepts were identified for potential Mars surface applications. A top-level characterization study was conducted to determine power system mass and area for each application. It is seen that PV systems are generally not suited for Mars surface applications due to the large surface area required and higher mass than a closed Brayton cycle SP100 reactor system. A reactor is currently being considered by NASA Lewis Research Center to provide power for base architectures including an ISRU (in situ resource utilization). An oxygen/methane powered heat engine would provide 40 kWe of emergency power for the habitat. A dynamic isotope power system (DIPS) is the current choice for a long-duration pressurized rover due to the excessive size of a PV/RFC system and higher mass of a heat engine system. DIPS has advantages for other low power systems due to its neatly immediate availability and flexibility (night or day power; no recharging required).<>
Keywords
Mars; fuel cells; heat engines; nuclear power; photovoltaic power systems; power supplies to apparatus; power systems; First Mars Outpost; Mars surface; NASA Lewis Research Center; Rocketdyne´s study; availability; chemical heat engine; closed Brayton cycle SP100 reactor; dynamic isotope power system; emergency power; flexibility; in situ resource utilization; isotope power; mission architecture; nuclear power; oxygen/methane powered heat engine; photovoltaic power; recharging; regenerative fuel cell; Electronics packaging; Heat engines; Inductors; Isotopes; Mars; NASA; Photovoltaic systems; Power system dynamics; Power systems; Solar power generation;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems Magazine, IEEE
Publisher
ieee
ISSN
0885-8985
Type
jour
DOI
10.1109/62.246041
Filename
246041
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