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Teleoperator maneuvering systemThe Teleoperator Maneuvering System (TMS) is a Shuttle launched, free-flying, remotely controlled reusable propulsive stage capable of performing spacecraft and payload placement services, retrieval functions, assembly/servicing support for large space systems, dexterous manipulator operations for planned or contingency satellite servicing, satellite viewing, and subsatellite science support. The basic TMS segments, subsystems and performance are described, beginning with the criteria and requirements derived from mission models. Examples of TMS benefits to the STS and user communities are demonstrated. TMS applications such as support and servicing of Space Station, materials processing and subsatellite missions are presented.
Document ID
19820062955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Turner, J. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
French, R. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Agan, W. E.
(Vought Corp. Dallas, TX, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1982
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 82-1817
Report Number: AIAA PAPER 82-1817
Meeting Information
Meeting: Space Systems Conference: The Space Transportation System: A Review of Its Present Capability and Probable Evolution
Location: Washington, DC
Start Date: October 18, 1982
End Date: October 20, 1982
Sponsors: AIAA, DGLR, AAS, and BIS,
Accession Number
82A46490
Distribution Limits
Public
Copyright
Other

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