节点文献
气动谐振管点火技术研究
Investigation on gas dynamic resonance tube ignition method
【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 ,给出了气动谐振管点火器工程设计的一般原则和相关参数的选择
【Abstract】 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.
【关键词】 液体推进剂火箭发动机;
点火;
点火系统;
气动加热;
【Key words】 Liquid propellant rocket engine; Ignition; Ignition system; Aerodynamic heating;
【Key words】 Liquid propellant rocket engine; Ignition; Ignition system; Aerodynamic heating;
【基金】 国家“八六三”基金资助项目 (86 3 2 3 4 7)
- 【文献出处】 推进技术 ,Journal of Propulsion Technology , 编辑部邮箱 ,2001年04期
- 【分类号】V434.1
- 【被引频次】11
- 【下载频次】172