This paper reports recently completed structural dynamics experimental activities with new ultra-lightweight 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: 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 eventually in-space deployment and performance of Gossamer spacecraft. Experimental research and development such as this is required to validate new analysis methods. The activities discussed in the paper are pathfinder accomplishments. conducted on unique components and prototypes of future spacecraft systems.
Structural Dynamics Experimental Activities in Ultra-Lightweight and Inflatable Space Structures
42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference ; 2001 ; Seattle, WA, United States
01.05.2001
Preprint
Keine Angabe
Englisch
British Library Conference Proceedings | 2001
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