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The numerical modelling of processes in combustion chambers of low thrust rocket engines
- Authors: Salich V.L.1
-
Affiliations:
- Institute of Mechanical Engineering
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 120-125
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6794
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-120-125
- ID: 6794
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Abstract
The mathematical model of processes in combustion chambers of low trust rocket engines with diphasic fuel compositions and results of calculations of the chamber of the engine with fuel composition gaseous oxygen / ethanol are presented.
About the authors
V. L. Salich
Institute of Mechanical Engineering
Author for correspondence.
Email: salich_vas@mail.ru
candidate of technical science
leading research engineer, head of research division
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