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Structural Dynamics Experimental Activities in Ultra-Lightweight and Inflatable Space StructuresThis paper reports recently completed structural dynamics experimental activities with new ultralightweight and inflatable space structures (a.k.a., "Gossamer" spacecraft) at NASA Langley Research Center, NASA Marshall Space Flight Center, and NASA Goddard Space Flight Center. Nine aspects of this work are covered, as follows: 1) inflated, rigidized tubes, 2) active control experiments, 3) photogrammetry, 4) laser vibrometry, 5) modal tests of inflatable structures, 6) in-vacuum modal tests, 7) tensioned membranes, 8) deployment tests, and 9) flight experiment support. Structural dynamics will play a major role in the design and eventual in-space deployment and performance of Gossamer spacecraft, and experimental R&D work such as this is required now to validate new analytical prediction methods. The activities discussed in the paper are pathfinder accomplishments, conducted on unique components and prototypes of future spacecraft systems.
Document ID
20010027549
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Pappa, Richard S.
(NASA Langley Research Center Hampton, VA United States)
Lassiter, John O.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Ross, Brian P.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2001-1263
Report Number: AIAA Paper 2001-1263
Meeting Information
Meeting: AIAA Gossamer Spacecraft Forum
Location: Seattle, WA
Country: United States
Start Date: April 16, 2001
End Date: April 19, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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