Software system for computing spacecraft aerodynamics
A.V. Kashkovsky, P.V. Vashchenkov, and M.S. Ivanov
Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
Pages: 73–84
Abstract
The field of application for the systems of high-altitude aerodynamics and typical problems solved are presented. The main requirements for these systems are formulated. Some methods for implementation of these requirements are shown by the example of RuSat system.
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