Forecasting the individual performance capabilities of the rocket engine powerplant units at the maintanance stage


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Abstract

This paper describes a methodology of calculation of the required performance capabilities of rocket engine power plant units.

About the authors

V. V. Biryuk

Samara State Aerospace University

Author for correspondence.
Email: Teplotex_ssau@bk.ru

Doctor of Sciences (Engineering)

Deputy Head of the Heat Engineering and Heat Engines Department

Russian Federation

V. M. Bronshtein

Samara State Aerospace University

Email: csdb@samtel.ru

Candidate of Sciences (Engineering)

Associate Professor of the Heat Engineering and Heat Engines Department

Russian Federation

A. S. Presnyakova

Samara State Aerospace University

Email: csdb@samtel.ru

Postgraduate Student of the Heat Engineering and Heat Engines Department

Russian Federation

M. Y. Shatilova

Samara State Aerospace University

Email: csdb@samtel.ru

Postgraduate Student of the Heat Engineering and Heat Engines Department

Russian Federation

S. S. Dostovalova

Samara State Aerospace University

Email: Teplotex_ssau@bk.ru

Undergraduate Student

Russian Federation

References

  1. Болотин, В.В. Ресурс машин и конструкций [Текст] / В.В. Болотин. – М.: Машиностроение, 1990. – 448 с.
  2. Основы создания агрегатов автоматики пневмогидравлических систем летательных аппаратов и двигателей. Ч. 1. Обеспечение конструкторской надежности и технологичности агрегатов [Текст] / А.И. Евстигнеев, А.Е. Жуковский, В.М. Квасов [и др.]. – Самара: НПО «Импульс», 1993. – 375 с.
  3. Эдельман, А.И. Топливные клапаны жидкостных ракетных двигателей [Текст] / А.И. Эдельман. – М.: Машиностроение, 1970. – 244 с.

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