航天推进技术研究院主办
[1]马冬英,卢 钢,张小平,等.液氧/甲烷燃气发生器试验研究[J].火箭推进,2013,39(03):21-26.
MA Dong-ying,LU Gang,ZHANG Xiao-ping,et al.Research on hot tests of LOX/methane gas generator[J].Journal of Rocket Propulsion,2013,39(03):21-26.
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MA Dong-ying,LU Gang,ZHANG Xiao-ping,et al.Research on hot tests of LOX/methane gas generator[J].Journal of Rocket Propulsion,2013,39(03):21-26.
液氧/甲烷燃气发生器试验研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
39
期数:
2013年03期
页码:
21-26
栏目:
研究与设计
出版日期:
2013-06-30
- Title:
- Research on hot tests of LOX/methane gas generator
- 文章编号:
- 1672-9374(2013)03-0021-06
- Keywords:
- liquid rocket engine; LOX/methane; gas generator; ignition; combus
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 为了研究液氧/甲烷的点火和燃烧特性，进行了液氧/甲烷燃气发生器热试验研究。介绍了液氧/甲烷燃气发生器热试验的试验装置、试验方案和试验情况，分析了试验结果。试验结果表明燃气发生器设计方案和点火方案可行，点火品质较好，能够在较宽的工作条件下稳定工作，燃烧组织合理，燃烧品质良好，温度均匀性较好，积碳轻微。
- Abstract:
- Hot firing tests of LOX/methane gas generator were researched for the characteristic of ignition and combustion of LOX/methane. In this paper, the testing apparatus, scheme and situation of LOX/methane gas generator for hot firing test were described, and the test results were analyzed. The tests results indicate that the design scheme and ignition procedure of the gas generator were feasible. The gas generator can work in a wide range of pressure and mixture ratio, and had rational combustion, good temperature uniformity and a little coking.
参考文献/References:
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[11]张小平,李春红,马冬英.液氧／甲烷发动机动力循环方式研究[J].火箭推进,2009,35(04):14.
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[12]仲伟聪.液氧/甲烷液体火箭发动机燃烧研究最新进展[J].火箭推进,2004,(01):52.
备注/Memo
收稿日期：2013-01-１３；修回日期：2013-02-17
基金项目：国家863项目（2007AA705302）
作者简介：马冬英（1981—），女，工程师，硕士，研究领域为液体火箭发动机系统设计
更新日期/Last Update:
1900-01-01