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Prototype solar power satellite optionsThe choice of options for the prototype solar power satellite is addressed relative to risk and cost. Emphasis is placed on the reduction of the risk of failure. Risk is the program cost multiplied by the reduction in probability of program success due to the risky action. Four classes of risk are identified. It is suggested that prototyping would reduce the technical risk as well as reduce the effects of the other three types of risk by allowing them to be quantified earlier. Prototype demonstration requirements addressed include electromagnetic power link feasibility demonstration, component integration verification, construction technology verification, and cost performance verification. Specific prototype requirements are listed and prototyping options are given in tabular form.
Document ID
19820014838
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sperber, B. R.
(Boeing Aerospace Co. Seattle, WA, United States)
Drexler, K. E.
(MIT)
Date Acquired
August 10, 2013
Publication Date
July 1, 1980
Publication Information
Publication: NASA, Washington The Final Proc. of the Solar Power Satellite Program Rev.
Subject Category
Energy Production And Conversion
Accession Number
82N22712
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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