Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block

Abstract

The pilot study of influence of the thermal stream simulating influence of the working mid-flight engine on parameters of liquid rocket engines of small draft is carried out. Operability of engines in the conditions of the propulsion system is confirmed, parameters of liquid rocket engines of small draft are defined and reserved before achievement of their limiting values on time and on temperature.

About the authors

Y. I. Ageenko

Isaev Chemical Machinery Design Bureau – Branch of Federal State Unitary Enterprise «Khrunichev State Research and Production Space Center»

Author for correspondence.
Email: kbhimmash@korolev-net.ru

Candidate of Technical Science

Chief Designer Lines, Head of the Liquid Rocket Engine of Small Thrust, Renowned Designer

Russian Federation

R. N. Galperin

Samara State Aerospace University

Email: ke_src@ssau.ru

Senior Research Fellow of the Research Center of Cosmic Energy

Russian Federation

Y. S. Ivashin

Samara State Aerospace University

Email: ke_src@ssau.ru

Candidate of Technical Science

Senior Research Fellow of the Research Center of Cosmic Energy

Russian Federation

V. E. Nigodjuk

Samara State Aerospace University

Email: ke_src@ssau.ru

Candidate of Technical Science

Associate Professor of the Department of Theory Engines Flight - Governmental Apparatus

Russian Federation

V. V. Ryzhkov

Samara State Aerospace University

Email: ke_src@ssau.ru

Candidate of Technical Science

Research Supervisor of the Research Center of Space Power

Russian Federation

A. V. Sulinov

Samara State Aerospace University

Email: ke_src@ssau.ru

Candidate of Technical Science

Associate Professor of the Department of Theory Engines Flight - Governmental Apparatus, Senior Research Fellow of the Research Center of Cosmic Energy

Russian Federation

References

  1. Дубинкин, Ю.М. Проблемы организации рабочего процесса жидкостных ракетных двигателей малой тяги [Текст] / Ю.М. Дубинкин, В.Е. Нигодюк // Известия ВУЗов. Авиационная техника. - 1993. - № 2. - С. 71-74.
  2. Нигодюк, В.Е Исследование закономерностей жидкофазного взаимодействия компонентов СЖРТ [Текст] / В.Е. Нигодюк, А.В. Сулинов // Вестник СГАУ. - 2009. - № 3 (19). – С. 316-321.
  3. Агеенко Ю.И. Исследование параметров смесеобразования и методический подход к расчетам и проектированию ЖРДМТ со струйно-центробежной схемой смешения компонентов АТ и НДМГ на стенке камеры сгорания [Текст] / Ю.И. Агеенко // Вестник СГАУ. - 2009. - № 3 (19). Ч.2. - С. 171-177.
  4. Фаворский, О. Н. Вопросы теплообмена в космосе [Текст]: изд. 2-е, доп.; учеб. пособие для вузов / О. Н.Фаворский, Я. С. Каданер. - Л.: Высшая школа, 1972. - 280 с.
  5. Основы теплопередачи в авиационной и ракетно-космической технике [Текст] / под ред. В.К. Кошкина. - М.: Машиностроение, 1975. - 623 с.

Statistics

Views

Abstract: 3392

PDF (Russian): 1807

Dimensions

PlumX

Refbacks

  • There are currently no refbacks.

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies