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Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation
- Authors: Dmitrenko A.I.1, Ivanov A.V.1, Rachuk V.S.1
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Affiliations:
- Design Bureau of Chemical Automation, Voronezh
- Issue: Vol 9, No 4 (2010)
- Pages: 38-48
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/941
- DOI: https://doi.org/10.18287/2541-7533-2010-0-4(24)-38-48
- ID: 941
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Abstract
The task of producing oxygen-hydrogen and oxygen-methane engines of the new generation designed without generators is urgent today. The turbopump unit is one of the main components of any engine. The paper is devoted to the development of turbopump unit design for engines without generators developed at the Design Bureau.
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About the authors
A. I. Dmitrenko
Design Bureau of Chemical Automation, Voronezh
Author for correspondence.
Email: cadb@comch.ru
Candidate of Technical Sciences
Chief Designer of Feed Systema
Russian FederationA. V. Ivanov
Design Bureau of Chemical Automation, Voronezh
Email: iav308@inbox.ru
Candidate of Technical Sciences
Deputy Chief Designer of Feed Systema
Russian FederationV. S. Rachuk
Design Bureau of Chemical Automation, Voronezh
Email: cadb@comch.ru
Doctor of Technical Sciences, Professor
General Director - General Designer
Russian FederationReferences
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