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Vibration resistance problem for a space vehicle with single-degree-of-freedom powered gyroscopes
- Authors: Filippov Y.I.1, Peresypkin K.V.2
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Affiliations:
- Space Rocket Centre “TsSKB-Progress”, Samara
- Samara State Aerospace University
- Issue: Vol 8, No 4 (2009)
- Pages: 72-79
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/836
- DOI: https://doi.org/10.18287/2541-7533-2009-0-4(20)-72-79
- ID: 836
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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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