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The integration of a mesh reflector to a 15-foot box truss structure. Task 3: Box truss analysis and technology developmentTo demonstrate the design and integration of a reflective mesh surface to a deployable truss structure, a mesh reflector was installed on a 15 foot box truss cube. The specific features demonstrated include: (1) sewing seams in reflective mesh; (2) mesh stretching to desired preload; (3) installation of surface tie cords; (4) installation of reflective surface on truss; (5) setting of reflective surface; (6) verification of surface shape/accuracy; (7) storage and deployment; (8) repeatability of reflector surface; and (9) comparison of surface with predicted shape using analytical methods developed under a previous task.
Document ID
19880009557
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bachtell, E. E.
(Martin Marietta Aerospace Denver, CO, United States)
Thiemet, W. F.
(Martin Marietta Aerospace Denver, CO, United States)
Morosow, G.
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1987
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:178228
MCR-86-669-TASK-3
NASA-CR-178228
Report Number: NAS 1.26:178228
Report Number: MCR-86-669-TASK-3
Report Number: NASA-CR-178228
Accession Number
88N18941
Funding Number(s)
CONTRACT_GRANT: NAS1-17551
PROJECT: RTOP 506-49-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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