Mathematical model of investigating normal acoustic modes of launch vehicle modules

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Abstract

The article presents a method which considers the influence of fuel and oxidizer tanks of a launch vehicle on sound propagation in the inter-tank space. An example of finding resonant acoustic modes and frequencies of a launch vehicle module and the analysis of sound-insulation characteristics of the module are also given.

About the authors

P. A. Popov

Space Rocket Center «TsSKB-Progress», Samara

Author for correspondence.
Email: banduir@rambler.ru

Chief of Group

Russian Federation

A. S. Belov

Space Rocket Center «TsSKB-Progress», Samara

Email: AnatoliyBelov@Gmail.com

Design Engineer

Russian Federation

A. N. Kryuchkov

Samara State Aerospace University

Email: kan@ssau.ru

Doctor of Technical Science

Professor of the Department of Automatic Systems of Power Installations

Russian Federation

References

  1. Исследования по повышению звукоизоляции самолетных конструкций (по материалам открытой зарубежной печати) [Текст]. - ЦАГИ, 1990. - 101 с.
  2. Экспериментальное определение звукоизоляции межбакового отсека блока III ступени РН "Союз" [Текст] / НТО, инв.№5535. - ЦАГИ, 1999. - 38 c.
  3. Владимиров, В. С. Уравнения математической физики [Текст] / В. С. Владимиров - М.: Наука, 1976. - 392 с.

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