Electromagnetic panel deployment and retraction in satellite missions

Author:

Inamori Takaya,Satou Yasutaka,Sugawara Yoshiki,Ohsaki Hiroyuki

Funder

JSPS KAKENHI

Hattori Hokokai Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. The rise of graphene;Geim;Nat. Mater.,2007

2. L. Herbeck, M. Leipold, Development and test of deployable ultra-lightweight cfrp-booms for a solar sail, in: Proceedings of the European Conference on Spacecraft Structures, Materials and Mechanical Testing, (0), Retrieved from: 〈http://adsabs.harvard.edu/full/2001ESASP.468..107H〉, 2000.

3. T. Inamori, K. Kishimoto, P. Saisutjarit, H. Ohsaki, Application of a magnetic planner actuator to extensible structure control in a Fuloshiki satellite, in: Proceedings of the Space Sciences and Technology Conference (n.d.), 2012.

4. T. Inamori, K. Kishimoto, P. Saisutjarit, H. Ohsaki, Application of magnetic planar actuators to control of extensible structures in small satellite missions, in: Proceedings of the Nagoya: UN/Japan Nano-Satellite Symposium, vol. 2008, 2012.

5. Elastic bending modulus of monolayer graphene;Lu;J. Phys. D: Appl. Phys.,2009

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