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The Space Technology 5 Power System DesignThe Space Technology 5 (ST5) mission is a NASA New Millennium Program (NMP) project that was developed to validate new technologies for future missions and to demonstrate the feasibility of building and launching multiple, miniature spacecraft that can operate as science probes, collecting research quality measurements. The three satellites in the ST5 constellation will be launched into a sun synchronous LEO (Low Earth Orbit) in early 2006. ST5 fits in the 25 kilogram and 24 Watt class of miniature but fully capable spacecraft. The power system design features the use of new technology components and a low voltage power bus. In order to hold the mass and volume low and to qualify new technologies for future use in space, high efficiency triple junction solar cells and a lithium ion battery were baselined into the design. The Power System Electronics (PSE) was designed for a high radiation environment and uses hybrid microcircuits for power switching and over current protection. The ST5 power system architecture and technologies will be presented.
Document ID
20050244973
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Stewart, Karen D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Hernandez-Pellerano, Amri I.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Communications And Radar
Report/Patent Number
ST5
Report Number: ST5
Meeting Information
Meeting: 3rd International Energy Conversion Engineering Conference
Location: San Francisco, CA
Country: United States
Start Date: August 15, 2005
End Date: August 18, 2005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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