ELECTRICAL COMPONENT TECHNOLOGY FOR 0.25 TO 10.0 MEGAWATT SPACE POWER SYSTEMS: DESIGN STUDY. Quarterly Technical Progress Report No. 1, September 1--November 30, 1966. Page: 16 of 165
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2. SCOPE OF STUDY
The scope of the Design Study is summarized in the following section
in order for the reader to better understand the extent of the work to be
carried out and the relationships of the various work described in the
following sections. There are three major tasks which contain a total of
twelve separate but closely interrelated sub-tasks as listed below.
Table 2. 1 Summary of Design Study Tasks
Parametric and Screening Studies
Power Uses and Missions Definition
Nuclear-Mechanical System Definition
Generator Parametric Study
AC Motor Parametric Study
Frequency Changer Parametric Study
Power Conditioning Parametric Study
Power Transmission and Distribution Study
Conceptual Design Analyses
Electrical System Definition
Conceptual Design Analysis and Layout
Experimental Verification (generator only)
Experimental Evaluation of Magnetic Unbalance
Forces and Flux Distribution
Experimental Evaluation of No-Load Losses
Experiments Associated with Rotor Cooling Concepts
Summary descriptions of the sub-tasks are presented below:
2.1 PARAMETRIC AND SCREENING STUDIES
2. 1. 1 Power Uses and Missions
The mission requirements and environmental conditions that affect
electrical component designs are included in the selection of the design
conditions for three classes of missions:5
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King, A.E. (ed.). ELECTRICAL COMPONENT TECHNOLOGY FOR 0.25 TO 10.0 MEGAWATT SPACE POWER SYSTEMS: DESIGN STUDY. Quarterly Technical Progress Report No. 1, September 1--November 30, 1966., report, January 1, 1967; United States. (https://digital.library.unt.edu/ark:/67531/metadc1021068/m1/16/: accessed March 28, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.