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New Design of Petal Type Deployable Space Mirror

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Multibody Mechatronic Systems

Part of the book series: Mechanisms and Machine Science ((Mechan. Machine Science,volume 25))

Abstract

A new kinematic design for a large petal-type space mirror package and deployment is considered. To check the approach computer and physical models of the multibody transformable structure were developed and studied. Results of simulation are presented in the paper.

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References

  1. http://www.asc.rssi.ru/radioastron

  2. http://www.asc.rssi.ru/millimetron

  3. http://www.jwst.nasa.gov

  4. http://safir.jpl.nasa.gov/whatIs.shtml

  5. Arkhipov MY, Baryshev AM, Kardashev NS et al (2008) Deployable antennas for space radio telescope: radioastron and millimetron missions. In: Proceedings of the 30th ESA antenna workshop. Noordwijk, Netherlands

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  8. Kardashev NS, Bujakas VI et al (2007) The millimetron project. Radioastrono- mical Tools and Techniques, Cambridge

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Correspondence to V. I. Bujakas .

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© 2015 Springer International Publishing Switzerland

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Bujakas, V.I. (2015). New Design of Petal Type Deployable Space Mirror. In: Ceccarelli, M., Hernández Martinez, E. (eds) Multibody Mechatronic Systems. Mechanisms and Machine Science, vol 25. Springer, Cham. https://doi.org/10.1007/978-3-319-09858-6_37

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  • DOI: https://doi.org/10.1007/978-3-319-09858-6_37

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-09857-9

  • Online ISBN: 978-3-319-09858-6

  • eBook Packages: EngineeringEngineering (R0)

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