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Testing a dual-mode ramjet engine with kerosene combustion

Testing a dual-mode ramjet engine with kerosene combustion 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. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Thermophysics and Aeromechanics Springer Journals

Testing a dual-mode ramjet engine with kerosene combustion

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Publisher
Springer Journals
Copyright
2015 Pleiades Publishing, Ltd.
ISSN
0869-8643
eISSN
1531-8699
DOI
10.1134/S0869864315050054
Publisher site
See Article on Publisher Site

Abstract

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.

Journal

Thermophysics and Aeromechanics – Springer Journals

Published: Sep 1, 2015

References

  • Gas-dynamic of flow structure in a channel under thermal and mechanical throttling
    V.M. Levin
  • Methodology of the experimental studies of ramjet combustion chamber operation at Moscow Aviation Institute
    V.M. Levin
  • Problems of implementing ramjet operation
    V.M. Levin