Technical and programmatic constraints in dynamic verification of satellite mechanical systems-Reference-Cited by-同舟云学术

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Technical and programmatic constraints in dynamic verification of satellite mechanical systems

Published:1996-01 Issue:1 Volume:38 Page:25-31
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Stavrinidis C.,Klein M.,Brunner O.,Newerla A.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference2 articles.

1. Establishment of vibration test input for experiment units from satellite system tests—lessons learned from the SOHO satellite;Stavrinidis,1994

2. Problems encountered in sine vibration testing of satellite with significant liquid mass;Brunner,1994

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1. DEVELOPMENT OF VIBRATION PROTECTION SYSTEMS OF SPACECRAFT — STATE OF THE ART AND PERSPECTIVES;Kosmìčna nauka ì tehnologìâ;2023-10-10

2. Classical and numerical approaches to determining V-section band clamp axial stiffness;Open Engineering;2014-01-15

3. Random Vibrations in Spacecraft Structures Design;Solid Mechanics and Its Applications;2009

4. Stress in V-section band clamps;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2004-03-01

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