Spacecraft structural test method based on kinematic excitation technique using verified finite element models
- Autores: Dolgikh EG1, Arhipkin YG1, Lysenko EA1, Lysenko КЕ1
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Afiliações:
- Edição: Volume 10, Nº 1-1 (2009)
- Páginas: 70-72
- Seção: Articles
- URL: https://journals.eco-vector.com/2712-8970/article/view/508312
- ID: 508312
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Texto integral
Resumo
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.
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Sobre autores
E Dolgikh
Email: zhendol@mail.ru
Y Arhipkin
E Lysenko
Email: vibro@iss-reshetnev.ru
К Lysenko
Email: atomgrad37@mail.ru