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Solar Sail Spacecraft Boom Vibration During Deployment and Damping Analysis
Date
2015-08-09
Author
Tekinalp, Ozan
Ataş, Ömer
Metadata
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URI
http://www.space-flight.org/
https://hdl.handle.net/11511/76294
Conference Name
AAS/AIAA ASTRODYNAMICS SPECIALIST CONFERENC, (9-13 August 2015)
Collections
Department of Aerospace Engineering, Conference / Seminar
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Boom deployment vibration analysis is presented for a solar sail 3U Cubesat. The damping of the boom vibration using shape memory alloys is examined. It is found that shape memory alloys do not reduce vibration below a certain level. Vibration damping via inherent friction in the deployment system is also considered. The analysis showed that the vibration may be completely damped due to the inherent friction in the deployment system.
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O. Tekinalp and Ö. Ataş, “Solar Sail Spacecraft Boom Vibration During Deployment and Damping Analysis,” presented at the AAS/AIAA ASTRODYNAMICS SPECIALIST CONFERENC, (9-13 August 2015), Vail, Colorado, United States Of America, 2015, Accessed: 00, 2021. [Online]. Available: http://www.space-flight.org/.