Research the influence of dispersions of stiffness and dissipative characteristics of design elements of the rocket on the accuracy of definition the flight loads
Автор: Seliverstov Alexander, Shevchenko Igor
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Актуальные проблемы машиностроения
Статья в выпуске: 1-2 т.16, 2014 года.
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In work results of calculated research the influence of dispersions of stiffness and dissipative characteristics of design elements of the rocket on the accuracy of definition the flight loads are stated. It is shown that for RC «Angara-A5» case loadings vary from the chosen dispersions of scatter rigidities no more, than for 10% of nominal.
Dynamic model, rocket, load, stiffness characteristic
Короткий адрес: https://sciup.org/148202780
IDR: 148202780
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