首页 | 本学科首页   官方微博 | 高级检索  
     

低温富燃火炬点火器研究
引用本文:孙纪国,王剑虹.低温富燃火炬点火器研究[J].导弹与航天运载技术,1999(6):17-22.
作者姓名:孙纪国  王剑虹
作者单位:北京液体火箭发动机研究所,北京
摘    要:火炬式电点火器在国外氢氧发动机上得到了广泛应用,介绍了对低温富燃火炬点火技术的初步研究情况,初步设计的火炬点火器试验件实现可靠的低温点火,并具有较广的工况和混合比较化范围。

关 键 词:点火器  火箭发动机  低温富燃  火炬式  氢氧发动机

Study on Cryogenic Fuel-Rich Spark Igniter
Sun Jiguo,Wang Jianhong.Study on Cryogenic Fuel-Rich Spark Igniter[J].Missiles and Space Vehicles,1999(6):17-22.
Authors:Sun Jiguo  Wang Jianhong
Abstract:Spark igniter is widely used in cryogenic liquid rocket engines in the world. A spark igniter has been successfully developed recently in China. The design and experimental research on the cryogenic fuel rich spark igniter are introduced in this paper. In the firing tests of the igniter, all the ignitions are successful without any misfire. Through these tests, the fundamental designs of the igniter are confirmed.
Keywords:Igniter  Low temperature  Rocket engine  
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号