| Citation: | CHEN Ruida, TIAN Zeng, CHEN Hongyu, et al. Effect of valve opening time difference on working process of 150 N hypergolic propellant liquid rocket engine[J]. Journal of Aerospace Power, 2024, 39（9）：20220683 doi: 10.13224/j.cnki.jasp.20220683
|
In order to study the effect of the valve opening time difference on the working process of the space liquid rocket engine using hypergolic propellants, the high-altitude simulated thermal test of a 150 N engine was carried out. The engine working stability, ignition thrust peak and response time were investigated when the oxidant valve and fuel valve were opened 40, 100, 500,
| [1] |
钱海涵,夏芳. 空间发动机真空起动点火时差及其实现方法[J]. 上海航天,1998,15(6): 28-32. QIAN Haihan,XIA Fang. The ingnition time difference and its realizable methods for spacecraft engine[J]. Aerospace Shanghai,1998,15(6): 28-32. (in Chinese
QIAN Haihan, XIA Fang. The ingnition time difference and its realizable methods for spacecraft engine[J]. Aerospace Shanghai, 1998, 15(6): 28-32. (in Chinese)
|
| [2] |
李平,王衍方. 四氧化二氮和肼推进剂点火过程的试验研究[J]. 火箭推进,1996,22(1): 1-5. LI Ping,WANG Yanfang. Experimental study on ignition process of nitrogen tetroxide and hydrazine propellants[J]. Journal of Rocket Propulsion,1996,22(1): 1-5. (in Chinese
LI Ping, WANG Yanfang. Experimental study on ignition process of nitrogen tetroxide and hydrazine propellants[J]. Journal of Rocket Propulsion, 1996, 22(1): 1-5. (in Chinese)
|
| [3] |
SUTTON G P. History of liquid propellant rocket engines in the United States[J]. Journal of Propulsion and Power,2003,19(6): 978-1007. doi: 10.2514/2.6942
|
| [4] |
俞肇铭. R-4D双组元姿控发动机的研制(四): 空间点火特性[J]. 现代防御技术,1982,10(5): 40-53. YU Zhaoming. Development of R-4D bicomponent attitude control engine (Ⅳ): space ignition characteristics[J]. Modern Defense Technology,1982,10(5): 40-53. (in Chinese
YU Zhaoming. Development of R-4D bicomponent attitude control engine (Ⅳ): space ignition characteristics[J]. Modern Defense Technology, 1982, 10(5): 40-53. (in Chinese)
|
| [5] |
刘昌国,陈锐达,刘犇,等. 小推力空间液体火箭发动机夹气启动特性[J]. 火箭推进,2021,47(3): 8-15. LIU Changguo,CHEN Ruida,LIU Ben,et al. Start-up characteristics of low-thrust space liquid rocket engine with entrained gas[J]. Journal of Rocket Propulsion,2021,47(3): 8-15. (in Chinese
LIU Changguo, CHEN Ruida, LIU Ben, et al. Start-up characteristics of low-thrust space liquid rocket engine with entrained gas[J]. Journal of Rocket Propulsion, 2021, 47(3): 8-15. (in Chinese)
|
| [6] |
杨立军,富庆飞. 液体火箭发动机推力室设计[M]. 北京: 北京航空航天大学出版社,2013.
|
| [7] |
蔡国飙,李家文,田爱梅,等. 液体火箭发动机设计[M]. 北京: 北京航空航天大学出版社,2011.
|
| [8] |
KIM B,HONG M,LEE J,et al. Experimental investigation on water hammer phenomenon in the recirculation line of a liquid rocket engine[J]. Journal of the Korean Society of Propulsion Engineers,2021,25(2): 110-118. doi: 10.6108/KSPE.2021.25.2.110
|
| [9] |
汪凤山,姚兆普,刘阳,等. 甲基肼/四氧化二氮发动机脉冲工况仿真与试验研究[J]. 空间控制技术与应用,2021,47(4): 56-62. WANG Fengshan,YAO Zhaopu,LIU Yang,et al. Numerical and experimental analysis of pulse mode characteristics in a MMH/NTO rocket engine[J]. Aerospace Control and Application,2021,47(4): 56-62. (in Chinese
WANG Fengshan, YAO Zhaopu, LIU Yang, et al. Numerical and experimental analysis of pulse mode characteristics in a MMH/NTO rocket engine[J]. Aerospace Control and Application, 2021, 47(4): 56-62. (in Chinese)
|
| [10] |
张黎辉,李家文,张雪梅,等. 航天器推进系统发动机动态特性研究[J]. 航空动力学报,2004,19(4): 546-549. ZHANG Lihui,LI Jiawen,ZHANG Xuemei,et al. Dynamic characteristics study of spacecraft propulsion system engine[J]. Journal of Aerospace Power,2004,19(4): 546-549. (in Chinese
ZHANG Lihui, LI Jiawen, ZHANG Xuemei, et al. Dynamic characteristics study of spacecraft propulsion system engine[J]. Journal of Aerospace Power, 2004, 19(4): 546-549. (in Chinese)
|
| [11] |
陈宏玉,刘红军,陈建华. 补燃循环发动机强迫起动过程[J]. 航空动力学报,2015,30(12): 3010-3016. CHEN Hongyu,LIU Hongjun,CHEN Jianhua. Forced start-up procedure of a staged combustion cycle engine[J]. Journal of Aerospace Power,2015,30(12): 3010-3016. (in Chinese
CHEN Hongyu, LIU Hongjun, CHEN Jianhua. Forced start-up procedure of a staged combustion cycle engine[J]. Journal of Aerospace Power, 2015, 30(12): 3010-3016. (in Chinese)
|
| [12] |
陈一丹,陈宏玉,刘亚洲. 液体火箭发动机汽蚀建模与低入口压力起动过程仿真[J]. 航空动力学报,2022,37(8): 1654-1663. CHEN Yidan,CHEN Hongyu,LIU Yazhou. Cavitation modeling and start-up under-rated pressure simulation of liquid rocket engine[J]. Journal of Aerospace Power,2022,37(8): 1654-1663. (in Chinese
CHEN Yidan, CHEN Hongyu, LIU Yazhou. Cavitation modeling and start-up under-rated pressure simulation of liquid rocket engine[J]. Journal of Aerospace Power, 2022, 37(8): 1654-1663. (in Chinese)
|
| [13] |
苏龙斐,张黎辉,潘海林. 卫星推进系统发动机启动过程数值仿真[J]. 航空动力学报,2005,20(4): 698-701. SU Longfei,ZHANG Lihui,PAN Hailin. Numerical simulation on the starting process of satellite propulsion system[J]. Journal of Aerospace Power,2005,20(4): 698-701. (in Chinese
SU Longfei, ZHANG Lihui, PAN Hailin. Numerical simulation on the starting process of satellite propulsion system[J]. Journal of Aerospace Power, 2005, 20(4): 698-701. (in Chinese)
|
| [14] |
巴延涛,侯凌云,毛晓芳,等. 甲基肼/四氧化二氮反应化学动力学模型构建及分析[J]. 物理化学学报,2014,30(6): 1042-1048. BA Yantao,HOU Lingyun,MAO Xiaofang,et al. Construction and analysis of a chemical kinetic model for monomethylhydrazine/nitrogen tetroxide reactions[J]. Acta Physico-Chimica Sinica,2014,30(6): 1042-1048. (in Chinese doi: 10.3866/PKU.WHXB201404093
BA Yantao, HOU Lingyun, MAO Xiaofang, et al. Construction and analysis of a chemical kinetic model for monomethylhydrazine/nitrogen tetroxide reactions[J]. Acta Physico-Chimica Sinica, 2014, 30(6): 1042-1048. (in Chinese) doi: 10.3866/PKU.WHXB201404093
|
| [15] |
KARIMI H,NASSIRHARAND A,BEHESHTI M. Dynamic and nonlinear simulation of liquid-propellant engines[J]. Journal of Propulsion and Power,2003,19(5): 938-944. doi: 10.2514/2.6187
|
| [16] |
戴佳,黄敏超,沈赤兵,等. 双组元液体挤压推进系统启动过程时序分析[J]. 火箭推进,2006,32(2): 16-22. DAI Jia,HUANG Minchao,SHEN Chibing,et al. Startup process timing analysis of liquid bipropellant pressure-fed propulsion system[J]. Journal of Rocket Propulsion,2006,32(2): 16-22. (in Chinese
DAI Jia, HUANG Minchao, SHEN Chibing, et al. Startup process timing analysis of liquid bipropellant pressure-fed propulsion system[J]. Journal of Rocket Propulsion, 2006, 32(2): 16-22. (in Chinese)
|
| [17] |
杨林涛,沈赤兵. 基于正交试验设计的姿控发动机起动特性[J]. 火箭推进,2019,45(5): 38-44. YANG Lintao,SHEN Chibing. Numerical analysis on starting characteristics of attitude control engine based on orthogonal test design method[J]. Journal of Rocket Propulsion,2019,45(5): 38-44. (in Chinese
YANG Lintao, SHEN Chibing. Numerical analysis on starting characteristics of attitude control engine based on orthogonal test design method[J]. Journal of Rocket Propulsion, 2019, 45(5): 38-44. (in Chinese)
|
| [18] |
杨林涛,沈赤兵. 小推力推进系统启动过程仿真分析[J]. 导弹与航天运载技术,2019(5): 48-52. YANG Lintao,SHEN Chibing. Simulation analysis on start process of low-thrust propulsion system[J]. Missiles and Space Vehicles,2019(5): 48-52. (in Chinese
YANG Lintao, SHEN Chibing. Simulation analysis on start process of low-thrust propulsion system[J]. Missiles and Space Vehicles, 2019(5): 48-52. (in Chinese)
|
| [19] |
于杭健,彭兢,舒燕,等. 月面高温下推力器可靠性试验[J]. 中国空间科学技术,2021,41(6): 123-131. YU Hangjian,PENG Jing,SHU Yan,et al. Thruster reliability experiment under high temperature on lunar surface[J]. Chinese Space Science and Technology,2021,41(6): 123-131. (in Chinese
YU Hangjian, PENG Jing, SHU Yan, et al. Thruster reliability experiment under high temperature on lunar surface[J]. Chinese Space Science and Technology, 2021, 41(6): 123-131. (in Chinese)
|
| [20] |
庄杰. 液体火箭发动机高空试验台研制[D]. 上海: 上海交通大学,2009. ZHUANG Jie. Design for liquid rocket engine high altitude test-bed[D]. Shanghai: Shanghai Jiao Tong University,2009. (in Chinese
ZHUANG Jie. Design for liquid rocket engine high altitude test-bed[D]. Shanghai: Shanghai Jiao Tong University, 2009. (in Chinese)
|
| [21] |
张奎好,王成刚. 变轨发动机大型高空模拟试验台[J]. 导弹与航天运载技术,2004(1): 57-60. ZHANG Kuihao,WANG Chenggang. Large altitude simulation test stand for orbit maneuver motor[J]. Missiles and Space Vehicles,2004(1): 57-60. (in Chinese
ZHANG Kuihao, WANG Chenggang. Large altitude simulation test stand for orbit maneuver motor[J]. Missiles and Space Vehicles, 2004(1): 57-60. (in Chinese)
|
| [22] |
李钰潼,王玫,谭紫阳,等. 低蒸汽压燃料与四氧化二氮自燃特性研究[J]. 西安交通大学学报,2022,56(6): 34-39. LI Yutong,WANG Mei,TAN Ziyang,et al. Study on hypergolic characteristics of low vapor pressure fuels and nitrous oxide[J]. Journal of Xi’an Jiaotong University,2022,56(6): 34-39. (in Chinese
LI Yutong, WANG Mei, TAN Ziyang, et al. Study on hypergolic characteristics of low vapor pressure fuels and nitrous oxide[J]. Journal of Xi’an Jiaotong University, 2022, 56(6): 34-39. (in Chinese)
|
| [23] |
李进华,孙兆懿. 四氧化二氮胶体饱和蒸气压的测试及分析[J]. 火炸药学报,2007,30(1): 74-77. LI Jinhua,SUN Zhaoyi. Test and analysis of the saturated vapor pressure of dinitrogen tetroxide colloid[J]. Chinese Journal of Explosives & Propellants,2007,30(1): 74-77. (in Chinese
LI Jinhua, SUN Zhaoyi. Test and analysis of the saturated vapor pressure of dinitrogen tetroxide colloid[J]. Chinese Journal of Explosives & Propellants, 2007, 30(1): 74-77. (in Chinese)
|
| [24] |
刘昌国,赵婷,姚锋,等. 第二代490 N轨控发动机研制及在轨飞行验证[J]. 推进技术,2020,41(1): 49-57. LIU Changguo,ZHAO Ting,YAO Feng,et al. Development and on-orbit flight verification of the second generation 490 N liquid apogee engine[J]. Journal of Propulsion Technology,2020,41(1): 49-57. (in Chinese
LIU Changguo, ZHAO Ting, YAO Feng, et al. Development and on-orbit flight verification of the second generation 490 N liquid apogee engine[J]. Journal of Propulsion Technology, 2020, 41(1): 49-57. (in Chinese)
|
| [25] |
刘昌国,赵婷,陈锐达,等. 星用490 N发动机喷注器局部燃气泄漏试验[J]. 航空动力学报,2021,36(3): 664-672. LIU Changguo,ZHAO Ting,CHEN Ruida,et al. Test on injector local gas leakage of 490 N engine for satellites[J]. Journal of Aerospace Power,2021,36(3): 664-672. (in Chinese
LIU Changguo, ZHAO Ting, CHEN Ruida, et al. Test on injector local gas leakage of 490 N engine for satellites[J]. Journal of Aerospace Power, 2021, 36(3): 664-672. (in Chinese)
|
DownLoad:
