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Peculiarities of acoustic loading of the space vehicle in the nose fairing launched as part of a «Soyuz»-type rocket
- Authors: Popov P.A.1, Sindyukov A.A.1, Kryuchkov A.N.1
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Affiliations:
- Samara State Space University named after academician S. P. Korolyov (National Research University)
- Issue: Vol 12, No 1 (2013)
- Pages: 80-90
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/125
- DOI: https://doi.org/10.18287/1998-6629-2013-0-1(39)-80-90
- ID: 125
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Abstract
The paper describes a method for finding resonant acoustic modes taking into account the influence of the spacecraft geometry and that of the nose fairing of the "Soyuz" rocket. An example of determining the resonant acoustic modes under the nose fairing is given. A method of determining the effects of spacecraft component density under the payload fairing on the acoustic loading is described. The analysis of acoustical characteristics of the nose fairing compartment is carried out taking into account the influence of cutouts of sound insulation elements. Recommendations on the reduction of acoustic loads on the upper surface of the spacecraft are given.
About the authors
P. A. Popov
Samara State Space University named after academician S. P. Korolyov (National Research University)
Author for correspondence.
Email: banduir@rambler.ru
Post-graduate Student of the Department of Automatic Systems of Power Installations
Russian FederationA. A. Sindyukov
Samara State Space University named after academician S. P. Korolyov (National Research University)
Email: sindyukovart@mail.ru
Post-graduate Student of the Department of Automatic Systems of Power Installations
Russian FederationA. N. Kryuchkov
Samara State Space University named after academician S. P. Korolyov (National Research University)
Email: kan@ssau.ru
Doctor of Technical Science, Professor
Professor of the Department of Automatic Systems of Power Installations
Russian FederationReferences
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