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Large space reflector technology on the Space StationThis paper discusses the role of the Space Station in the evolutionary development of large space reflector technology and the accommodation of mission systems which will apply large space reflectors during the late 1990s and the early part of the next century. Reflectors which range from 10 to 100 meters in size and which span the electromagnetic spectrum for applications that include earth communications, earth observations, astrophysics and solar physics, and deep space communications are discussed. The role of the Space Station in large space reflector technology development and system performance demonstration is found to be critical; that role involves the accommodation of a wide variety of technology demonstrations and operational activities on the Station, including reflector deployment and/or assembly, mechanical performance verification and configuration refinement, systematic diagnostics of reflector surfaces, structural dynamics and controls research, overall system performance characterization and modification (including both radio frequency field pattern measurements and required end-to-end system demonstrations), and reflector-to-spacecraft integration and staging. A unique facility for Space Station-based, large space reflector research and development is proposed. A preliminary concept for such a Space Station-based Large Space Reflector Facility (LSRF) is described.
Document ID
19860064816
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mankins, J. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dickinson, R. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Freeland, R. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Marzwell, N. I.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1986
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-2302
Accession Number
86A49554
Distribution Limits
Public
Copyright
Other

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