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An economic analysis of a commercial approach to the design and fabrication of a space power systemThis paper discusses a commercial approach to the design and fabrication of an economical space power system. With the advent of the space shuttle, steps can be taken to back away from the presently used space qualified approach in order to reduce cost of space hardware by incorporating, where possible, commercial design, fabrication, and quality assurance methods. Cost reductions are projected through the conceptual design of a 2 kW space power system built with the capability for having serviceability. The approach to system costing that has been used takes into account both the constraints of operation in space and commercial production engineering approaches. The cost of this power system reflects a variety of cost/benefit tradeoffs that would reduce system cost as a function of system reliability requirements, complexity, and the impact of rigid specifications. A breakdown of the system design, documentation, fabrication and reliability and quality assurance cost estimates are detailed.
Document ID
19790050724
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Putney, Z.
(Solarex Corp. Rockville, Md., United States)
Been, J.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 79-0914
Meeting Information
Meeting: Conference on Advanced Technology for Future Space Systems
Location: Hampton, VA
Start Date: May 8, 1979
End Date: May 10, 1979
Accession Number
79A34737
Distribution Limits
Public
Copyright
Other

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