Abstract
This paper presents a concept for cylindrical deployable space structures (CDSSs) and their geometrical properties. To construct large structures in space environment automatically, many concepts for deployable structures have been proposed to satisfy the requirements of the limited allowable space in the launching vehicle that transports these structures to orbit.
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References
Rauschenbach, “Solar Cell Array Design Handbook,” Van Nostrand Reinhold, 1980.
Pellegrino, S., “Large Retractable Appendages in Spacecraft,” J. of Spacecraft and Rockets, Vol. 32, No. 6, pp. 1006–1014, 1995.
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© 2000 Springer Science+Business Media Dordrecht
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Sogame, A., Furuya, H. (2000). Conceptual Study on Cylindrical Deployable Space Structures. In: Pellegrino, S., Guest, S.D. (eds) IUTAM-IASS Symposium on Deployable Structures: Theory and Applications. Solid Mechanics and Its Applications, vol 80. Springer, Dordrecht. https://doi.org/10.1007/978-94-015-9514-8_40
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DOI: https://doi.org/10.1007/978-94-015-9514-8_40
Publisher Name: Springer, Dordrecht
Print ISBN: 978-90-481-5539-2
Online ISBN: 978-94-015-9514-8
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