电邮这篇文章 Spacecraft structural test method based on kinematic excitation technique using verified finite element models
- 作者: Dolgikh EG1, Arhipkin YG1, Lysenko EA1, Lysenko КЕ1
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隶属关系:
- 期: 卷 10, 编号 1-1 (2009)
- 页面: 70-72
- 栏目: Articles
- URL: https://journals.eco-vector.com/2712-8970/article/view/508312
- ID: 508312
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详细
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.
作者简介
E Dolgikh
Email: zhendol@mail.ru
Y Arhipkin
E Lysenko
Email: vibro@iss-reshetnev.ru
К Lysenko
Email: atomgrad37@mail.ru
参考
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