On the stress-strain state of film structures in space at electrodynamic deployment

Details On the stress-strain state of film structures in space at electrodynamic deployment On the stress-strain state of film structures in space at electrodynamic deployment

Dec 2007

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2007cosre..45..506s&link_type=abstract

Cosmic Research, Volume 45, Issue 6, pp.506-512

Computer Science

46.25.Hf

Scientific paper

We discuss a possibility of using the Ampere force for deployment and stabilization of film structures in space. It is supposed that a conductor connected with a power supply is deposited on the surface of a thin film, or solar batteries are used as conductors with current. The stress and strain of the thin film, caused by the electric current flow over a circular conductor confining this film, are found. The method of calculating the radial component of the stress tensor in a film, connected with concentric circular conductors with current, is obtained. The distribution of stresses for a film with three conductors is calculated. A possibility of minimizing the magnetic moment of a system of currents is discussed.

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