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This paper describes the results of studies related to conceptual topologies of an integrated utility-like space power system. The system topologies are comparatively analyzed by considering their transmission energy losses as functions of mainly distribution voltage level and load composition. The analysis is expedited by use of a Distribution System Analysis and Simulation (DSAS) software. This recently developed computer program by the Electric Power Research Institute (EPRI) uses improved load models to solve the power flow within the system. However, present shortcomings of the software with regard to space applications, and incompletely defined characteristics of a space power system make the results applicable to only the fundamental trends of energy losses of the topologies studied. Accountability, such as included, for the effects of the various parameters on the system performance can constitute part of a planning tool for a space power distribution system.

One driving factor that is critical to aerospace power electronic systems is the reduction in weight and size. A key focus of power electronic building blocks (PEBB) is the reduction of size and weight and, hence, increased integration of power electronic systems. PEBB can be viewed as a three-port electronic module with input, output and control ports. This paper summarizes the results of a study undertaken by NASA Glenn Research Center to evaluate the insertion of PEBB into aerospace power electronic systems. It surveys the applications of power electronics in aerospace systems, and evaluates the capabilities and limitations of potential PEBB architectures for aerospace applications. It, also, constructs a road map to assist in formulating requirements and developing architectures for aerospace-based PEBB product development. Finally, it identifies follow-on work for detailed research to expedite first generation aerospace-based PEBB product developments.