摘要
本文着重介绍了阿里安的第Ｖ１８次飞行事故之后ＨＭ７Ｂ的点火器的改进情况，同时还介绍ＨＭ６０的点火器的研制情况，并简单地介绍日本和美国的一些氢氧火箭发动机的点火器及其点火极限。
The igniter improvements for Ariane third stage HM7B engine after the V18 flight failure are discussed in this paper. The development status of HM60 igniter, and the ignition limits of various LOX-LH_2 rocket engines such as LE-5, RL-10 and J-2 are also described.
出处
《导弹与航天运载技术》
1994年第5期32-42,共11页
Missiles and Space Vehicles
