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Docking-mechanism attenuator with electromechanical damperTheoretical and practical problems involved in the application of electromechanical damping for spacecraft docking-mechanism attenuation are discussed. Some drawbacks of hydraulic dampers used for the purpose are pointed out. The basic scheme of the attenuator with the electromechanical damper is given.
Document ID
19720005748
Document Type
Other
Authors
Syromyatnikov, V. S. (Academy of Sciences (USSR) Moscow, Ussr)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publication: NASA. Goddard Space Flight Center 5th Aerospace Mech. Symp.
Subject Category
SPACE VEHICLES
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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