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Large diameter astromast development, phase 1Coilable-longeron lattice columns called Astromasts (trademark) were manufactured for a variety of spacecraft missions. These flight structures varied in diameter from 0.2 to 0.5 meter (9 to 19 in.), and the longest Astromast of this type deploys to a length of 30 meters (100 feet). A double-laced diagonal Astromast design referred to as the Supermast (trademark) which, because it has shorter baylengths than an Astromast, is approximately four times as strong. The longeron cross section and composite material selection for these structures are limited by the maximum strain associated with stowage and deployment. As a result, future requirements for deployable columns with high stiffness and strength require the development of both structures in larger diameters. The design, development, and manufacture of a 6.1-m-long (20-ft), 0.75-m-diameter (30-in.), double-laced diagonal version of the Astromast is described.
Document ID
19830019795
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Preiswerk, P. R.
(Astro Research Corp. Carpinteria, CA, United States)
Finley, L. A.
(Astro Research Corp. Carpinteria, CA, United States)
Knapp, K.
(Astro Research Corp. Carpinteria, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 30, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:170781
NASA-CR-170781
ARC-TN-11119
Report Number: NAS 1.26:170781
Report Number: NASA-CR-170781
Report Number: ARC-TN-11119
Accession Number
83N28066
Funding Number(s)
CONTRACT_GRANT: NAS8-34547
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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