NDLI: Development and ground testing of a compactly stowed scalable inflatably deployed solar sail

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Development and ground testing of a compactly stowed scalable inflatably deployed solar sail

Content Provider	NASA Technical Reports Server (NTRS)
Author	Lichodziejewski, David Mann, Troy Slade, Kara Reinert, Rich Belvin, Keith Derbes, Billy
Copyright Year	2004
Description	This paper discusses the solar sail design and outlines the interim accomplishments to advance the technology readiness level (TRL) of the subsystem from 3 toward a technology readiness level of 6 in 2005. Under Phase II of the program many component test articles have been fabricated and tested successfully. Most notably an unprecedented section of the conically deployed rigidizable sail support beam, the heart of the inflatable rigidizable structure, has been deployed and tested in the NASA Goddard thermal vacuum chamber with good results. The development testing validated the beam packaging and deployment. The inflatable conically deployed, Sub Tg rigidizable beam technology is now in the TRL 5-6 range. The fabricated masses and structural test results of our beam components have met predictions and no changes to the mass estimates or design assumptions have been identified adding great credibility to the design. Several quadrants of the Mylar sail have also been fabricated and successfully deployed validating our design, manufacturing, and deployment techniques.
File Size	21844961
Page Count	16
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20040071043
Archival Resource Key	ark:/13960/t44r2vh30
Language	English
Publisher Date	2004-04-19
Access Restriction	Open
Subject Keyword	Solar Sails Ground Tests Dynamic Tests Technology Assessment Mylar Trademark Product Development Inflatable Space Structures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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