Testing a dual-mode ramjet engine with kerosene combustion

Results of life firing tests of a dual-mode ramjet engine intended for operation in the speed range М = 3−6 are discussed. The tests were carried out on a test bench under freestream conditions typical of Mach 6 flight at 27.6-km altitude. In the tests, the adopted design and technological solutions...

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Bibliographic Details
Published in:Thermophysics and aeromechanics 2015-09, Vol.22 (5), p.569-574
Main Authors: Levin, V. M., Karasev, V. N., Kartovitskii, L. L., Krymov, E. A., Skachkov, O. A.
Format: Article
Language:English
Subjects:
Physics
Physics and Astronomy
Thermodynamics
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Summary:Results of life firing tests of a dual-mode ramjet engine intended for operation in the speed range М = 3−6 are discussed. The tests were carried out on a test bench under freestream conditions typical of Mach 6 flight at 27.6-km altitude. In the tests, the adopted design and technological solutions were verified, and efficient operation of the ramjet engine with kerosene combustion during 110 s was demonstrated.
ISSN:0869-8643
1531-8699
DOI:10.1134/S0869864315050054