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Solar power satellite construction conceptsIn-space construction of a photovoltaic solar power satellite that is 5 1/2 by 25 km in size and weighs 81,000 tons is discussed. One of the construction approaches being considered requires 1/8-size power collection satellite modules to be constructed in low earth orbit (LEO) and transported to geosynchronous orbit (GEO) using self-powered electric thrusters. At GEO, these 1/8-size modules are connected and the antenna is constructed and attached. This construction approach will require about 300 people at LEO and 380 people at GEO working 10 hour shifts for 90 day staytimes. This paper describes the construction operations and construction equipment. Also discussed are some of the human factors considerations.
Document ID
19780052796
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Miller, K. H.
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Astronautics (General)
Report/Patent Number
AAS 77-203
Report Number: AAS 77-203
Meeting Information
Meeting: Annual Meeting
Location: San Francisco, CA
Start Date: October 18, 1977
End Date: October 20, 1977
Accession Number
78A36705
Funding Number(s)
CONTRACT_GRANT: NAS9-15196
Distribution Limits
Public
Copyright
Other

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