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Next steps in space transportation and operationsDesign of a 25-kW power or utilities module, capable of extending the effective duration of Spacelab missions, is discussed. The power module, planned for availability in 1984, could also support a Spacelab modified to be a free-flyer by providing attitude control and power. In addition, development of a 250-kW power module to support a Shuttle-tended space platform or a Shuttle-tended space construction base is projected. A free-flying teleoperator capable of deboosting Skylab, systems to construct large planar arrays in space, and a habitable module providing crew quarters for continuously manned operations are also described.
Document ID
19780035634
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Disher, J. H.
(NASA Office of Space Transportation Systems Washington, D.C., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: Astronautics and Aeronautics
Volume: 16
Subject Category
Space Transportation
Accession Number
78A19543
Distribution Limits
Public
Copyright
Other

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