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Teleoperator maneuvering systemThe teleoperator maneuvering system (TMS), consisting of the vehicle, the shuttle orbiter bay cradle with airborne support equipment, and the aft flight deck control station, is described. The vehicle is a reusable remotely controlled free flying vehicle capable of a variety of missions including payload placement, retrieval, servicing, viewing, and large space systems assembly support. The TMS flies preprogrammed trajectories as well as being controlled or reprogrammed from the aft flight deck or the ground. A building block design philosophy is described which permits the evolution of capability as it is needed and delays cost as much as possible. Various mission operations are discussed.
Document ID
19830002910
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Turner, J. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Publication Information
Publication: NASA. Johnson Space Center Satellite Serv. Workshop, Vol. 1
Subject Category
Space Transportation
Accession Number
83N11180
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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