Ignition system for combustion chambers operating on air+kerosene propellants

1Marchan, RA
1Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Kosm. nauka tehnol. 2003, 9 ;(Supplement1):128-132
https://doi.org/10.15407/knit2003.01s.128
Publication Language: Russian
Abstract: 
Wc present results of experimental investigations of igniters using thermal effects in a resonance tube. The best characteristics are obtained for the igniter that uses burning of a part of fuel in the resonance cavity in order to intensify warming up of the igniting surface.
References: 
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3. Przirembel C. E. G., Fletcher L. S. Aerothermodynamics of a Simple Resonance Tube. Raketnaja tehnika i kosmonavtika, 15 (1) (1977) [in Russian].