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|
|Publication Language: Russian|
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.
1. Sources of powerful ultrasound. Part 1 (Nauka, Moscow, 1967) [in Russian].
2. Kuptsov V. M., Ostroukhova S. I., Filippov K. N. Pressure fluctuations and heating of a gas by the inflow of a supersonic jet into a cylindrical cavity. Izvestiia AN SSSR, Mekhanika Zhidkosti i Gaza, 12 (5) 104—111 (1977) [in Russian].
3. Przirembel C. E. G., Fletcher L. S. Aerothermodynamics of a Simple Resonance Tube. Raketnaja tehnika i kosmonavtika, 15 (1) (1977) [in Russian].