Testing a dual-mode ramjet engine with kerosene combustion
V.M. Levin1, V.N. Karasev1, L.L. Kartovitskii1, E.A. Krymov2, and O.A. Skachkov2
1Moscow Aviation Institute (National Research University), Moscow, Russia
2Bardin Central Research Institute of Ferrous Metallurgy, Moscow, Russia
E-mail: vadimlevin@yahoo.com
Keywords: dual-mode ramjet engine, kerosene, firing tests
Pages: 569–574
Abstract
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.
DOI: DOI: 10.1134/S0869864315050054
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