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Development of and dynamic studies concerning a cable boom system prototypeThe conception of a cable boom system for a scientific spin stabilized satellite led to a flat cable stowed on a drum with a flexlead without conversion to avoid slip rings and to facilitate automatic restowage from any state of deployment. Some dynamic features of the extended cable boom and especially the comparison between round and flat cables were investigated in a phenomenological study using a test rig capable of inducing lateral, torsional and thermal cycling disturbances separately or in any combination.
Document ID
19740003556
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bring, G.
(European Space Agency. European Space Research and Technology Center ESTEC, Noordwijk, Netherlands)
Schmidt, G.
(Dornier-Werke G.m.b.H. Bristol, United States)
Wyn-Roberts, D.
(British Aircraft Corp.)
Date Acquired
August 7, 2013
Publication Date
October 1, 1973
Publication Information
Publication: NASA. Langley Res. Center The 8th Aerospace Mech. Symp.
Subject Category
Machine Elements And Processes
Accession Number
74N11669
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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