Rocket Engine with Continuous Film Detonation of Liquid Fuel

It was experimentally proven for the first time that it is possible to perform continuous detonation combustion of a film of a liquid fuel in the annular combustor of a demonstrator of a liquid-fuel detonation rocket engine. Firing tests revealed a near-limit mode of longitudinally pulsating film de...

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Bibliographic Details
Published in:Doklady. Physical chemistry (1991) 2018-08, Vol.481 (2), p.105-109
Main Authors: Frolov, S. M., Shamshin, I. O., Aksenov, V. S., Sadykov, I. A., Gusev, P. A., Zelenskii, V. A., Evstratov, E. V., Alymov, M. I.
Format: Article
Language:English
Subjects:
Chemistry
Chemistry and Materials Science
Combustion chambers
Detonation waves
Fuels
Liquid fuels
Physical Chemistry
Rocket engines
Rocket firing
Rockets
Test firing
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Summary:It was experimentally proven for the first time that it is possible to perform continuous detonation combustion of a film of a liquid fuel in the annular combustor of a demonstrator of a liquid-fuel detonation rocket engine. Firing tests revealed a near-limit mode of longitudinally pulsating film detonation and modes of continuous spinning film detonation with one and two detonation waves circulating within the annular gap of the combustor.
ISSN:0012-5016
1608-3121
DOI:10.1134/S0012501618080018