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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
- Authors: Ageenko Y.I.1, Galperin R.N.2, Ivashin Y.S.2, Nigodjuk V.E.2, Ryzhkov V.V.2, Sulinov A.V.2
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Affiliations:
- Isaev Chemical Machinery Design Bureau – Branch of Federal State Unitary Enterprise «Khrunichev State Research and Production Space Center»
- Samara State Aerospace University
- Issue: Vol 11, No 3-3 (2012): Special Issue
- Pages: 251-259
- Section: CONFERENCE MATERIALS
- URL: https://journals.ssau.ru/vestnik/article/view/2240
- DOI: https://doi.org/10.18287/2541-7533-2012-0-3-3(34)-251-259
- ID: 2240
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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 FederationR. N. Galperin
Samara State Aerospace University
Email: ke_src@ssau.ru
Senior Research Fellow of the Research Center of Cosmic Energy
Russian FederationY. 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 FederationV. 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 FederationV. 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 FederationA. 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 FederationReferences
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