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Space Shuttle Tail Service Mast Concept VerificationDesign studies and analyses were performed to describe the loads and dynamics of the space shuttle tail service masts (TSMs). Of particular interest are the motion and interaction of the umbilical carrier plate, lanyard system, vacuum jacketed hoses, latches, links, and masthead. A development test rig was designed and fabricated to obtain experimental data. The test program is designed to (1) verify the theoretical dynamics calculations, (2) prove the soundness of design concepts, and (3) elucidate problem areas (if any) in the design of mechanisms and structural components. Design, fabrication, and initiation of TSM development testing at Kennedy Space Center are described.
Document ID
19760021185
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Uda, R. T.
(Planning Research Corp. Los Angeles, CA, United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Publication Information
Publication: JPL 10th Aerospace Mech. Symp.
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
76N28273
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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