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Solar thermal upper stage: Economic advantage and development statusA solar thermal upper stage (STUS) is envisioned as a propulsive concept for the future. The STUS will be used for low Earth orbit (LEO) to geostationary-Earth orbit (GEO) transfer and for planetary exploration missions. The STUS offers significant performance gains over conventional chemical propulsion systems. These performance gains translate into a more economical, more efficient method of placing useful payloads in space and maximizing the benefits derived from space activity. This paper will discuss the economical advantages of an STUS compared to conventional chemical propulsion systems, the potential market for an STUS, and the recent activity in the development of an STUS. The results of this assessment combined with the performance gains, will provide a strong justification for the development of an STUS.
Document ID
19960001209
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Adams, Alan M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-111062
NAS 1.15:111062
Report Number: NASA-TM-111062
Report Number: NAS 1.15:111062
Accession Number
96N11216
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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