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Hybrid deployable support truss designs for LDRConcepts for a 20-meter diameter Large Deployable Reflector (LDR) deployable truss backup structure, and analytical predictions of its structural characteristics are discussed. The concept shown is referred to as the SIXPAC; It is a combination of the PACTRUSS concept and a single-fold beam, which would make up the desired backup structure. One advantage of retaining the PACTRUSS concept is its packaging density and its capability for synchronous deployment. Various 2-meter hexagonal panel arrangements are possible for this Hybrid PACTRUSS structure depending on the panel-to-structure attachment strategies used. Static analyses of the SIXPAC using various assumptions for truss designs and panel masses of 10 kg sq meters were performed to predict the tip displacement of the structure when supported at the center. The tip displacement ranged from 0.20 to 0.44 mm without the panel mass, and from 0.9 to 3.9 mm with the panel mass (in a 1-g field). The data indicate that the structure can be adequately ground tested to validate its required performance in space, assuming the required performance in space is approximately 100 microns. The static displacement at the tip of the structure when subjected to an angular acceleration of 0.001 rad/sec squared were estimated to range from 0.8 to 7.5 microns, depending on the type of truss elements.
Document ID
19900004169
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hedgepeth, J.
(Astro Aerospace Corp. Santa Barbara, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 15, 1988
Publication Information
Publication: Jet Propulsion Lab., California Inst. of Tech., Report of the Asilomar 3 LDR Workshop
Subject Category
Engineering (General)
Accession Number
90N13485
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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