摘要
为了发展液体火箭发动机的气动谐振管非电点火新技术 ,提出了一种新颖的组合喷嘴混气谐振加热方案 ,并介绍了所研制的氦气谐振热表面点火器和同轴氢氧谐振火炬点火器 。
To develop the new technology of gas dynamic resonance tube non-electric ignition for liquid rocket engines, a new conceptual scheme of combined nozzle mixing gas resonance heating was proposed. The gaseous helium resonance surface heating igniter and the co-axial gaseous oxygen-hydrogen resonance torch igniter were described. And the general engineering design criteria for the resonance tube igniter were proposed.
出处
《推进技术》
EI
CAS
CSCD
北大核心
2001年第4期286-289,共4页
Journal of Propulsion Technology
基金
国家"八六三"基金资助项目 (86 3 2 3 4 7)
