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Satellite Power Systems (SPS) Space Transportation Workshop SummarySpace transportation requirements are major elements in the technical and economic realization of the entire SPS concept. First, steps in enhancing the shuttle include the Titan based liquid boost module (LBM) and liquid propellant boosters (LPB) to replace the present solid rocket boosters (SRB). The next choice between new ballistic or winged boosters must still be made; as well as the choice between series (staged) and parallel operation. Entirely new vehicles of large size are required before the economic and environmental problems of the prototype, or even demonstration, SPS can be resolved. Social impacts such as noise, and atmospheric pollution, locally and in the ionosphere, must be fully addressed. Although rather advanced technology and well developed operational management is required to properly target the average cost of gross cargo payloads into LEO at 30 $ (1979)/kg for the construction of the initial SPS, the further goal for repetitive construction of 30 to 60 SPS at 15 $ (1979)/kg for all operational payloads require the use of very advanced, long lived vehicles with a sophisticated operational organization using off shore, equatorial launch sites.
Document ID
19820014836
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Layton, J. P.
(Layton (J. Preston) Princeton Junction, NJ, United States)
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
82N22710
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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