Application of a magnetohydrodynamic element in the control loop of a rotating spacecraft with cavities partially filled with liquid

Details Application of a magnetohydrodynamic element in the control loop of a rotating spacecraft with cavities partially filled with liquid Application of a magnetohydrodynamic element in the control loop of a rotating spacecraft with cavities partially filled with liquid

Jun 2008

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2008cosre..46..251n&link_type=abstract

Cosmic Research, Volume 46, Issue 3, pp.251-263

Physics

45.20.Dc

Scientific paper

This paper is a continuation of [1 3] and a generalization of the results for a rotating spacecraft with cavities partially filled with liquid and equipped with an operational magnetohydrodynamic (MHD) element in the loop of its attitude control. This element makes possible the creation of hingeless systems of stabilization and orientation that do not require rocket propellant consumption. The application of an MHD element is considered for stabilization in the mode of spin-up of a spacecraft not having gyroscopic stability.

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