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Approaches to the evaluation of fuels for hypersonic engines
- Authors: Sergeev S.M.1, Petrukhin N.V.2
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Affiliations:
- “25 State Scientific and Research Institute of Chemmotology of the Russian Ministry of Defense”, Moscow
- 25-th State Research Institute of Chemmotology, Ministry of Defence of Russian Federation
- Issue: Vol 12, No 3-2 (2013): Vestnik SSAU
- Pages: 181-184
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/1840
- DOI: https://doi.org/10.18287/1998-6629-2013-0-3-2(41)-181-184
- ID: 1840
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Abstract
The article presents gas flow parameters in four cross- sections of the engine at the flight speed of 8M at the altitude of 20 km for various hydrocarbon fuels. The data were obtained with the use of a multi-purpose program complex. The analysis of the obtained results allowed determining the level of requirements for the basic properties of fuels for hyper-sonic ramjet engines and arguments in favour of developing a new fuel for hypersonic ram-flow jet engines as well as new methods for its evaluation.
About the authors
S. M. Sergeev
“25 State Scientific and Research Institute of Chemmotology of the Russian Ministry of Defense”, Moscow
Author for correspondence.
Email: ssm.58@mail.ru
Candidate of Science (Engineering), Associate Professor
Head of Laboratory
Russian FederationN. V. Petrukhin
25-th State Research Institute of Chemmotology, Ministry of Defence of Russian Federation
Email: 25gosniihim@mail.ru
Doctor of Science (Engineering), Professor
Chief Researcher
Russian FederationReferences
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