A modular PMAD system for small spacecraft
Author(s) -
Robert M. Button
Publication year - 1997
Publication title -
space technology and applications international forum (staif - 97)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.1063/1.52117
Subject(s) - modular design , spacecraft , converters , series and parallel circuits , aerospace , computer science , electrical engineering , voltage , photovoltaic system , electric power system , power (physics) , electronic engineering , engineering , aerospace engineering , physics , quantum mechanics , operating system
Current trends in satellite design are focused on developing small, reliable, and inexpensive spacecraft. To that end, a modular power management and distribution system (PMAD) is proposed which will help transition the aerospace industry towards an assembly line approach to building spacecraft. The modular system is based on an innovative DC voltage boost converter called the Series Connected Boost Unit (SCBU). The SCBU uses existing DC-DC converters and adds a unique series connection. This simple modification provides the SCBU topology with many advantages over existing boost converters. Efficiencies of 94–98%, power densities above 1,000 We/kg, and inherent fault tolerance are just a few of the characteristics presented. Limitations of the SCBU technology are presented, and it is shown that the SCBU makes an ideal photovoltaic array regulator. A modular design based on the series connected boost unit is outlined and functional descriptions of the components are given.
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