Vibration resistance problem for a space vehicle with single-degree-of-freedom powered gyroscopes

Abstract


Vibration resistance of a space vehicle is estimated in terms of the values of equipment vibration amplitudes. The procedure of estimation is presented as applied to a space vehicle subject to vibrations caused by residual back of balance of powered gyroscopes.


About the authors

Yu. I. Filippov

Space Rocket Centre “TsSKB-Progress”, Samara

Author for correspondence.
Email: fyui@samtel.ru

Russian Federation

K. V. Peresypkin

Samara State Aerospace University

Email: peresypkin@mail.ru

Russian Federation

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