Comparative Evaluation of the Two Methods of Determining the Unsteady Aerodynamic Characteristics of Cylindrical Patterns Separated Parts of Launch Vehicles for Space Purposes

Ecology and security clearance of cargo into Earth orbit space considered in unsteadyaerodynamics of the separated parts of of launch vehicles for space applications, which directly involves the definition of the shape and size of fields separated by falling parts, fragmentation issues and software...

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Bibliographic Details
Main Authors: A. I. Khlupnov, A. Yu. Galaktionov
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2017-02-01
Series:Aèrokosmičeskij Naučnyj Žurnal
Subjects:
Online Access:https://aerospace.elpub.ru/jour/article/view/57