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Shuttle/tethered satellite systemA tethered satellite system was conceived as a device to extend the capability of the Space Shuttle to perform scientific/applications investigations and operational activities. The concept envisions a multiple-use tethered system with closed-loop control, capable of supporting a payload or satellite suspended from the Shuttle cargo bay, toward or away from the Earth, at distances up to 100 kilometers from the Shuttle. The background and results of early analyses and feasibility studies are discussed and a design and operational description of the system are presented. Also presented are a discussion of potential applications of the Tethered Satellite System, and plans for an operational verification flight in 1982.
Document ID
19810020955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rupp, C. C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Laue, J. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1978
Publication Information
Publication: Alabama Univ. UAH(NASA Workshop on the Use of a Tethered Satellite System
Subject Category
Space Transportation
Meeting Information
Meeting: Goddard Memorial Symp.
Location: Washington, DC
Country: United States
Start Date: March 8, 1978
End Date: March 10, 1978
Accession Number
81N29493
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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