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Adaptation and Re-Use of Spacecraft Power System Models for the Constellation ProgramNASA's Constellation Program is embarking on a new era of space exploration, returning to the Moon and beyond. The Constellation architecture will consist of a number of new spacecraft elements, including the Orion crew exploration vehicle, the Altair lunar lander, and the Ares family of launch vehicles. Each of these new spacecraft elements will need an electric power system, and those power systems will need to be designed to fulfill unique mission objectives and to survive the unique environments encountered on a lunar exploration mission. As with any new spacecraft power system development, preliminary design work will rely heavily on analysis to select the proper power technologies, size the power system components, and predict the system performance throughout the required mission profile. Constellation projects have the advantage of leveraging power system modeling developments from other recent programs such as the International Space Station (ISS) and the Mars Exploration Program. These programs have developed mature power system modeling tools, which can be quickly modified to meet the unique needs of Constellation, and thus provide a rapid capability for detailed power system modeling that otherwise would not exist.
Document ID
20080043624
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Hojnicki, Jeffrey S.
(NASA Glenn Research Center Cleveland, OH, United States)
Kerslake, Thomas W.
(NASA Glenn Research Center Cleveland, OH, United States)
Ayres, Mark
(Hamilton-Sundstrand Space, Land and Sea Canoga Park, CA, United States)
Han, Augustina H.
(Hamilton-Sundstrand Space, Land and Sea Windsor Locks, CT, United States)
Adamson, Adrian M.
(Deep Space Systems, Inc. Littleton, CO, United States)
Date Acquired
August 24, 2013
Publication Date
September 1, 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/TM-2008-215425
E-16594
AIAA Paper 2008-5616
Report Number: NASA/TM-2008-215425
Report Number: E-16594
Report Number: AIAA Paper 2008-5616
Meeting Information
Meeting: Sixth International Energy Conversion Engineering Conference (IECEC)
Location: Cleveland, OH
Country: United States
Start Date: July 28, 2008
End Date: July 30, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 644423.06.32.03.05.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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