Spacecraft structural test method based on kinematic excitation technique using verified finite element models
Автор: Dolgikh E.G., Arhipkin Y. g, Lysenko E.A., Lysenko К.Е.
Журнал: Сибирский аэрокосмический журнал @vestnik-sibsau
Рубрика: Авиационная и ракетно-космическая техника
Статья в выпуске: 1-1 (22), 2009 года.
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The problem of spacecraft structure ground static strength tests insufficiency is discussed in the paper. The additional spacecraft structure strength tests by means of kinematic excitation method has been carried out.
Static strength tests, kinematical excitation, verification finite element model
Короткий адрес: https://sciup.org/148175809
IDR: 148175809
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