| Citation: | WU Jing, SUN Wei, CAI Guo-biao. Simulation and experiment for preheating process of N2O monopropellant thruster with inner-heater[J]. Journal of Aerospace Power, 2013, 28(3): 556-560.
|
| [1] |
Chigier N,Gemci T.A review of micro propulsion technology[R].AIAA-2003-670,2003.
|
| [2] |
Reichbach J G,Sedwick R J,Martinez-Sanchez M.Micropropulsion system selection for precision formation flying satellites[R].AIAA-2001-3646,2001.
|
| [3] |
贾永刚,赵勇,汤海滨.微推进技术及研究发展现状[C]//中国宇航学会年固体火箭推进剂第22届年会论文集.成都:中国宇航学会,2005:242-248.
|
| [4] |
Zakiov V,Zhang H.A model for the operation of nitrous oxide monopropellant[J].Aerospace Science And Technology,2008,12(4):318-323.
|
| [5] |
Tiliakos N,Tyll J S.Development and testing of a nitrous oxide/propane rocket engine[R].AIAA-2001-3258,2001.
|
| [6] |
禹天福,贾月.一氧化二氮催化分解的研究与应用[J].化学推进剂与高分子材料,2006,4(2): 6-10. YU Tianfu,JIA Yue.Research and application on the catalytic decomposition of nitrous oxide[J].Chemical Propellants and Polymeric Materials,2006,4(2):6-10.(in Chinese)
|
| [7] |
孙威,方杰,张佳,等.N2O单组元推力器预热过程有限元分析[J].航空动力学报,2009,24(9):2152-2156. SUN Wei,FANG Jie,ZHANG Jia,et al.Finite element analysis on preheating process of N2O monopropellant thruster[J]. Journal of Aerospace Power,2009,24(9):2152-2156.(in Chinese)
|
| [8] |
霍雪亮,韦迪,李路明.N2O单组元推进器预热过程的建模[J].推进技术,2005,26(1):80-83. HUO Xueliang,WEI Di,LI Luming.Modeling of N2O monopropellant thruster pre-heating[J].Journal of Propulsion Technology,2005,26(1):80-83.(in Chinese)
|
| [9] |
方杰,田辉,蔡国飙.N2O单组元微推进系统及其喷管流场的初步研究[J].推进技术,2005,26(6):495-498. FANG Jie,TIAN Hui,CAI Guobiao.Preliminary study on a N2O micro propulsion system and its nozzle flow field[J].Journal of Propulsion Technology,2005,26(6):495-498.(in Chinese)
|
| [10] |
孙威,方杰,蔡国飙,等.N2O单组元微推力器性能分析及试验[J].北京航空航天大学学报,2008,34(12):1469-1472. SUN Wei,FANG Jie,CAI Guobiao,et al.Performance analysis and experimental research on nitrous oxide monopropellant micro-thruster[J].Jounal of Beijing University of Aeronautics and Astronautics,2008,34(12):1469-1472.(in Chinese)
|
| [11] |
孙威,方杰,郑力铭,等.N2O微推力器性能及喷管热结构分析[J].火箭推进,2008,34(5):5-9. SUN Wei,FANG Jie,ZHENG Liming,et al.N2O micro-thruster performance and the nozzle thermo-structure analysis[J].Journal of Rocket Propulsion,2008,34(5):5-9.(in Chinese)
|
| [12] |
沈军,刘伟强,汤建华.单组元发动机推力室在轨温度数值仿真[J].推进技术,2003,24(3):201-203. SHEN Jun,LIU Weiqiang,TANG Jianhua.Numerical simulation for temperature in a monopropellant thrust chamber on the orbit[J].Journal of Propulsion Technology,2003,24(3):201-203.(in Chinese)
|
| [13] |
韩乐,李茂,方杰,等.N2O单组元微推力器真空试验设计与分析[J].航空动力学报,2011,26(10):2358-2363. HAN Yue,LI Mao,FANG Jie,et al.Vacuum experiment study on a N2O monopropellant micro-thruster[J].Journal of Aerospace Power,2011,26(10):2358-2363.(in Chinese)
|
| [14] |
李茂,韩乐,方杰,等.N2O单组元微推力器高空模拟实验研究[J].推进技术,2011,32(3):307-311. LI Mao,HAN Yue,FANG Jie,et al.Simulated altitude experimental investigation for N2O monopropellant micro-thruster[J].Journal of Propulsion Technology,2011,32(3):307-311.(in Chinese)
|
| [15] |
马庆芳.使用热物理性质手册[M].北京:中国农业机械出版社,1986.
|
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