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Structural assembly demonstration experimentThe experiment is of an operational variety, designed to assess crew capability in Large Space System (LSS) assembly. The six Structural Assembly Demonstration Experiment objectives include: (1) the establishment of a quantitative correlation between LSS neutral buoyancy simulation and on-orbit assembly operations in order to enhance the validity of those assembly simulations; (2) the quantitative study of the capabilities and mechanics of human assembly in an Extravehicular Activity environment; (3) the further corroboration of the LSS Assembly Analysis cost algorithm through the obtainment of hard data base information; (4) the verification of LSS assembly techniques and timeless, as well as the identification of crew imposed loads and assembly aid requirements and concepts; (5) verification of a Launch/Assembly Platform structure concept for other LSS missions; and (6) lastly, to advance thermal control concepts through a flexible heat pipe.
Document ID
19820011408
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stokes, J. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: NASA. Langley Research Center Large Space Systems Technol., Pt. 2, 1981
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
82N19282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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