Spacecraft structural test method based on kinematic excitation technique using verified finite element models
- Авторлар: Dolgikh EG1, Arhipkin YG1, Lysenko EA1, Lysenko КЕ1
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Мекемелер:
- Шығарылым: Том 10, № 1-1 (2009)
- Беттер: 70-72
- Бөлім: Articles
- URL: https://journals.eco-vector.com/2712-8970/article/view/508312
- ID: 508312
Дәйексөз келтіру
Толық мәтін
Аннотация
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.
Негізгі сөздер
Авторлар туралы
E Dolgikh
Email: zhendol@mail.ru
Y Arhipkin
E Lysenko
Email: vibro@iss-reshetnev.ru
К Lysenko
Email: atomgrad37@mail.ru