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Increasing the efficiency and stability of fuel supply to the combustion chamber of a liquid rocket engine by spray nozzles
- Authors: Ageenko Y.I.1, Bubnova A.S.1
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Affiliations:
- Technological University named after twice Hero of the Soviet Union Pilot-Cosmonaut A.A. Leonov
- Issue: Vol 23, No 2 (2024)
- Pages: 7-13
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/27637
- DOI: https://doi.org/10.18287/2541-7533-2024-23-2-7-13
- ID: 27637
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Abstract
In this paper, various configurations of jet nozzles are analyzed, as well as their design. The effects of the inlet chamfer of jet nozzles on their flow rate and range are considered. It is shown out that today it is expedient to make precision micro-holes of the nozzles using high-precision three-dimensional electric-erosion equipment. The optimal design parameters of jet nozzles are also determined.
About the authors
Yu. I. Ageenko
Technological University named after twice Hero of the Soviet Union Pilot-Cosmonaut A.A. Leonov
Author for correspondence.
Email: yi.ageenko@mail.ru
Doctor of Science (Engineering), Professor of the Department of Engineering and Technology
Russian FederationA. S. Bubnova
Technological University named after twice Hero of the Soviet Union Pilot-Cosmonaut A.A. Leonov
Email: annette.bubnova@mail.ru
ORCID iD: 0009-0008-1912-6400
Student of the Department of Engineering and Technology
Russian FederationReferences
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