Email this article Spacecraft structural test method based on kinematic excitation technique using verified finite element models
- Authors: Dolgikh EG1, Arhipkin YG1, Lysenko EA1, Lysenko КЕ1
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Affiliations:
- Issue: Vol 10, No 1-1 (2009)
- Pages: 70-72
- Section: Articles
- URL: https://journals.eco-vector.com/2712-8970/article/view/508312
- ID: 508312
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Abstract
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.
About the authors
E G Dolgikh
Email: zhendol@mail.ru
Y G Arhipkin
E A Lysenko
Email: vibro@iss-reshetnev.ru
К Е Lysenko
Email: atomgrad37@mail.ru
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