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Nikolay Nerovny

Publications and source records attributed to Nikolay Nerovny.

3 recordsLinked to original sources

Nanosatellite aerobrake maneuvering device

In this paper, we present the project of the heliogyro solar sail unit for deployment of CubeSat constellation and satellite deorbiting. The ballistic calculations show that constellation deployment period can vary from 0.18 years for 450km initial orbit and 2 CubeSats up to 1.4 years for 650km initial orbit and 8 CubeSats. We also describe the structural and electrical design of the unit and consider aspects of its integration into a standard CubeSat frame.

astro-ph.IM

Light radiation pressure upon an optically orthotropic surface

In this paper, we discuss the problem of determination of light radiation pressure force upon an anisotropic surface. The optical parameters of such a surface are considered to have major and minor axes, so the model is called an orthotropic model. We derive the equations for force components from emission, absorption, and reflection, utilizing a modified Maxwell's specular-diffuse model. The proposed model can be used to model a flat solar sail with wrinkles. By performing Bayesian analysis for example of a wrinkled surface, we show that there are cases in which an orthotropic model of the optical parameters of a surface may be more accurate than an isotropic model.

physics.class-ph

Representation of light pressure resultant force and moment as a tensor series

In this article we address a problem of determination of light pressure upon space structures of the complex geometric shape. For the surface element, we wrote a condition that this element can interact with light only from the front side, not from the back side. This condition To in the form of series of Chebyshev polynomials of the first kind. Chebyshev expansion lets us move to the series of tensors of increasing rank for the problem of determination of force and moment. We obtained expressions for the fiber method for determination of light pressure on space structures of complex geometry taking into account self--shadowing and reflections within the structure. We also give the expressions for tensor parametrization by the specularity coefficient in case of specular-diffuse reflection. For these expressions we calculated the principal moment and force upon two-sided flat solar sail, spherical and cylindrical bodies, and approximated light pressure upon a perspective space observatory Millimetron. The proposed expressions can be used in the ballistic analysis of solar sails and other space objects, which are significantly affected by the radiation pressure. Also, these results can be used to analyze the dynamics of movement of large-scale space structures around the center of gravity under the light pressure.

astro-ph.IM