Application of a modified generalized sail model on a solar sail with wrinkles

Author:

Nerovny Nikolay,Lapina Irina

Funder

Russian Foundation for Basic Research

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference41 articles.

1. Alhorn, D., Casas, J., Agasid, E., Adams, C., Laue, G., Kitts, C., O’Brien, S., 2011. NanoSail-D: The Small Satellite That Could! (SSC11-VI-1). In: Presentation at AIAA/USU Conference on Small Satellites, Utah State University, Logan, Utah, USA, 2011. http://digitalcommons.usu.edu/smallsat/2011/all2011/37.

2. Ancona, E., Kezerashvili, R.Y., 2016. Orbital dynamics of a solar sail accelerated by thermal desorption of coatings. arXiv preprint arXiv:1609.03131, 2016. http://arxiv.org/abs/1609.03131.

3. Bar-Sever, Y., Kuang, D., 2004. New empirically derived solar radiation pressure model for global positioning. In: System Satellites, IPN Progress Report, pp. 42–159.

4. Campbell, B.A., Thomas, S.J., 2014. Realistic solar sail thrust. In M. Macdonald, editor, Advances in Solar Sailing, pages 407–435. Springer, Berlin Heidelberg, Berlin, Heidelberg, 2014. ISBN 978-3-642-34906-5 978-3-642-34907-2. doi: 10.1007/978-3-642-34907-2_27. .

5. Differential equation for the amplitude of wrinkles;Epstein;AIAA J.,2003

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