Dynamics of Spring-Deployed Solar Panels for Agile Nanospacecraft

Author:

Santoni Fabio1

Affiliation:

1. Dipartimento di Ingegneria Astronautica, Elettrica ed Energetica (DIAEE), Università di Roma “la Sapienza”, Via Salaria 851, 00138 Rome, Italy.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference38 articles.

1. Alminde L. and Laursen K. K. (2009). “A strategic approach to developing space capabilities using CubeSat technology.” Proc. 4th Int. Conf. on Recent Advances in Space Technologies 2009 RAST ‘09 IEEE New York 43–47.

2. Calassa M. C. and Kackley R. (1995). “Solar array deployment mechanism.” Proc. 29th Aerospace Mechan. Symp. NASA 79–93.

3. Campbell D. et al. (2006). “Development of a novel passively deployed roll-out solar array.” Proc. 2006 IEEE Aerospace Conf. IEEE New York.

4. Miniaturized attitude control system for nanosatellites

5. Clark C. and Kirk S. (2012). “Off-the-shelf deployable solar panels for CubeSats.” CubeSat Developers’ Workshop 2012 Cal Poly San Luis Obispo CA.

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