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液氧/甲烷燃气发生器点火方案研究
引用本文:李春红,张小平,马冬英,徐浩海.液氧/甲烷燃气发生器点火方案研究[J].火箭推进,2010,36(5):7-12.
作者姓名:李春红  张小平  马冬英  徐浩海
作者单位:西安航天动力研究所,陕西,西安,710100
基金项目:国家航天技术支撑项目 
摘    要:在对比化学点火、火药点火及电火花点火优缺点的基础上,选取了技术成熟、点火可靠的火药点火用于液氧/甲烷燃气发生器热试。用黑火药点燃固体推进剂的点火药量计算公式估算了火药点火药量,给出了液氧/甲烷燃气发生器火药点火器的其它参数。根据液氧/甲烷推进剂特点,确定了火药燃气-液氧-甲烷依次进入燃气发生器的点火时序。成功进行了4次液氧/甲烷燃气发生器热试,结果表明:液氧/甲烷燃气发生器点火起动过程平稳,点火品质较好,点火方案合理,适于较宽工作条件下的液氧/甲烷点火。

关 键 词:液氧/甲烷  燃气发生器  点火方案

Ignition scheme of LOX/methane gas generator
LI Chun-hong,ZHANG Xiao-ping,MA Dong-ying,XU Hao-hai.Ignition scheme of LOX/methane gas generator[J].Journal of Rocket Propulsion,2010,36(5):7-12.
Authors:LI Chun-hong  ZHANG Xiao-ping  MA Dong-ying  XU Hao-hai
Institution:LI Chun-hong,ZHANG Xiao-ping,MA Dong-ying,XU Hao-hai (Xi'an Aerospace Propulsion Institute,Xi'an 710100,China)
Abstract:The solid cartridge igniter was chosen for the ignition of LOX/methane gas generator in comparison with chemical and electric igniter.The parameters of the igniter were set by the calculation formula and experience of designing similar igniters.The time sequence of LOX/methane gas generator ignition was determined according to the characteristic of LOX/methane propellant.Four firing tests of LOX/methane gas generator were performed successfully.There was no sharp pressure peak or temperature peak appeared i...
Keywords:LOX/methane  gas generator  ignition scheme  
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