PDF下载 分享
[1]李 强,王菊金.补燃循环过氧化氢/煤油发动机性能敏感性分析[J].火箭推进,2013,39(05):35-40.
 LI Qiang,WANG Ju-jin.Analysis of performance sensitivity of hydrogen peroxide/kerosene staged-combustion engine[J].Journal of Rocket Propulsion,2013,39(05):35-40.
点击复制

补燃循环过氧化氢/煤油发动机性能敏感性分析

参考文献/References:

[1]ANDERSON W, CROCKETT D, HILL S, et al. Low cost propulsion using a high-density, storable, and clean propellant combination, AIAA 98-3679[R]. USA: AIAA, 1998.
[2]BUTLER K. AR2-3 Engine refurbishment and gas gener- ator testing, AIAA 99-2738 [R]. USA: AIAA, 1999.
[3]VENTURA M, GARBODEN G. A brief history of conc- entrated hydrogen peroxide uses, AIAA 99-2739[R]. USA: AIAA, 1999.
[4]VENTURA M, MULLENS P. The use of hydrogen per- oxide for propulsion and power, AIAA 99-2880[R]. USA: AIAA, 1999.
[5]VENTURA M, WERNIOMONT E. History of the reaction motors super performance 90% H2O2/kerosene LR-40 rocket engine, AIAA 2001-3838[R]. USA: AIAA, 2001.
[6]KIM P Y, MAJAMAKI A, PAPESH C, et al. Design and development testing of the TR-108-a 30klbf-thrust-class hydrogen peroxide/hydrocarbon pump-fed engine, AIAA 2005-3566[R]. USA: AIAA, 2005.
[7]AKRKHANGELSKY V I, SUDAKOV V S, FATUEV I Y. History of development of hydrogen peroxide LPRE at NPO Energomash, IAC-05-E4.3.01[R]. USA: IAF, 2005.
[8]郑大勇, 颜勇, 张卫红. 氢氧火箭发动机性能敏感性分析[J]. 火箭推进, 2011, 37(4): 18-23.
[9]高允彦. 正交试验及回归试验设计方法[M]. 北京: 冶金工业出版社, 1988.
[10]董李亮. 过氧化氢发动机试验技术现状[J].火箭推进, 2004, 30(6): 36-39.
[11]侯金丽, 金平, 蔡国飙. 基于敏感性分析的氧/甲烷燃烧反应简化机理[J]. 航空动力学报, 2012, 27(7): 114-119.
[12]凌前程. 过氧化氢双组元发动机推力室研究[J]. 火箭推进, 2009, 35(4): 25-29.

相似文献/References:

[1]陈宏玉,刘红军.补燃循环发动机推力调节过程建模与仿真研究[J].火箭推进,2014,40(01):18.
 CHEN Hong-yu,LIU Hong-jun.Modeling and simulations on the thrust regulation process of staged combustion cycle rocket engine[J].Journal of Rocket Propulsion,2014,40(05):18.
[2]李 程,杨永强,徐浩海,等.500 t级液氧煤油补燃发动机起动过程仿真研究[J].火箭推进,2014,40(06):1.
 LI Cheng,YANG Yong-qiang,XU Hao-hai,et al.Numerical simulation of start-up process for 500 t thrust LOX/kerosene staged combustion cycle rocket engine[J].Journal of Rocket Propulsion,2014,40(05):1.
[3]党锋刚,马红宇,李春红,等.液氧煤油发动机稳态故障仿真分析[J].火箭推进,2012,38(02):27.
 DANG Feng-gang,MA Hong-yu,LI Chun-hong,et al.Steady-state fault simulation and effect analysis of LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2012,38(05):27.
[4]李 强,聂 嵩,刘业奎,等.过氧化氢/煤油发动机推力室气液燃烧数值模拟[J].火箭推进,2011,37(04):35.
 LI Qiang,NIE Song,LIU Ye-kui,et al.Numerical simulation of combustion characteristicsfor thrust chamber in hydrogen peroxide/kerosene engine[J].Journal of Rocket Propulsion,2011,37(05):35.
[5]杨永强,刘红军,徐浩海,等.补燃循环发动机强迫起动研究[J].火箭推进,2011,37(02):14.
 YANG Yong-qiang,LIU Hong-jun,XU Hao-hai,et al.Research on forced start-up of staged combustion engine[J].Journal of Rocket Propulsion,2011,37(05):14.
[6]张小平.补燃循环发动机推力调节研究[J].火箭推进,2008,34(04):1.
 Zhang Xiaoping.lnvestlgatlon on the thrust regulation of staged combustmn cycle engine[J].Journal of Rocket Propulsion,2008,34(05):1.
[7]徐浩海,刘站国.补燃循环发动机起动过程涡轮功率控制[J].火箭推进,2006,32(04):10.
 Xu Haohai,Liu Zhanguo.Turbine power control of staged combustion cycle engine during start-up[J].Journal of Rocket Propulsion,2006,32(05):10.
[8]张小平,丁丰年,刘站国,等.补燃循环发动机推进剂利用系统研究[J].火箭推进,2005,31(02):7.
 Zhang Xiaoping,Ding Fengnian,Liu Zhanguo,et al.Investigation of propellant utilization system for staged combustion rocket engine[J].Journal of Rocket Propulsion,2005,31(05):7.
[9]段小龙,刘站国,王拴虎,等.补燃循环液体火箭发动机大范围工况调节方案研究[J].火箭推进,2004,(03):1.
[10]王鹏武.全流量补燃循环液氧/甲烷发动机系统分析[J].火箭推进,2004,(06):15.
 Wang Pengwu.Analysis of FFSCC LOX/Methane Rocket Engine System[J].Journal of Rocket Propulsion,2004,(05):15.

备注/Memo

收稿日期:2013-04-24;修回日期:2013-08-24
基金项目:国家863项目(2009AA706309)
作者简介:李强(1981—),男,高级工程师,博士,研究领域为液体火箭发动机

更新日期/Last Update: 1900-01-01