[1]贾艳辉,张天平,李小平.离子推力器加速栅寿命概率性分析[J].推进技术,2011,32(6):766769
Jia Y H, Zhang T P,Li X P. Probabilistic evaluation of ion thruster accelerator grid life[J]. Journal of Propulsion Technology, 2011,32(6):766769
[2]Chien K R, Hart S L, Tighe W G, et al. L3 communications ETI electric propulsion overview[R].IEPC2005315,2005
[3]Kajiwara K, Ikeda M, Kohata H, et al. ETSⅧ ion engine and its operation on orbit[R]. IEPC2009048, 2009
[4]Killinger R, Leiter H, Kukies R. RITA ion propulsion sytems for commercial and scientific applications[R]. AIAA20075200, 2007
[5]Brophy J R, Plok J E, Randolph T M, et al. Lifetime qualification of electric thrusters for deep space missions [R]. AIAA20085184, 2008
[6]贾艳辉,李忠明,张天平,等. 等离子体密度对栅极系统束流影响的数值分析[J]. 中国空间科学技术,2012, 32(3):7277
Jia Y H, Li Z M, Zhang T P, et al. Numerical simulation of the effect of plasma density on beam extraction character for grid system[J].Chinese Space Science and Technology,2012, 32(3):7277
[7]贾艳辉,张天平,李小平,等. 离子推力器加速栅主要失效模式分析[C].第七届中国电推进技术学术研讨会,深圳,2011
Jia Y H, Zhang T P, Li X P, et al. The key failure mode analysis of ion thruster accelerator [C]. The 7th Chinese Electric Propulsion Conference, Shenzhen, 2011
[8]郭宁,江豪成,高军,等.离子发动机空心阴极失效形式分析[J].真空与低温,2005,11(4):239242
Guo N, Jiang H C, Gao J, et al. Analisis of ion thruster hollow cathode failure mode [J].Vacuum & Cryogenics, 2005,11(4):239242
[9]贾艳辉.LIPS200离子推力器寿命预测和评价研究[D].北京:中国空间技术研究院,2012
Jia Y H. Service life analysis and assessment for LIPS200 ion thruster [D]. Beijing: China Academy of Space Technology, 2012
[10]Kaufman H R. Technology of electronbombardment ion thruster [J].Advances in Electronics and Electron Physics, 1974, 36:265373
[11]张天平. 高性能电推进技术的发展和应用[C].卫星系统推进技术研讨会,银川,2012
Zhang T P. Developing and applications of high performance electric propulsion [C]. Propulsion Technology of Satellite System Conference, Yinchuan, 2012
[12]贾艳辉,张天平,郑茂繁,等. 离子推力器栅极系统电子反流阈值的数值分析[J].推进技术,2012,33(6):991996
Jia Y H, Zhang T P, Zheng M F, et al. Electron backstreaming accelerator grid limited voltage numerical evolution for 20cm Xe ion thruster grid system[J]. Journal of Propulsion Technology, 2012,33(6):991996
[13]郑茂繁,江豪成,顾左,等.20cm氙离子推力器3000h寿命实验[J]. 航天器环境工程,2009,8(4):374377
Zheng M F, Jiang H C, Gu Z, et al. 3000 h life test of 20cm Xe ion thruster [J]. Spacecraft Environment Engineering, 2009, 8(4):374377
[14]贾艳辉,张天平. 20cm氙离子推力器加速栅寿命预测[J]. 真空与低温,2010, 16(4): 208213
Jia Y H, Zhang T P. The service life assessment of 20cm Xe ion thruster accelerate grid [J]. Vacuum & Cryogenics, 2010,16(4):208213
[15]Peng X H, Ruyten W M, Keefer D, et al. Chargeexchange grid erosion study for groundbased and spacebased operations of ion thrusters[R]. IEPC1993173,1993
[16]张天平,刘乐柱,贾艳辉.电推进系统空心阴极产品试验技术[J].火箭推进,2010,36(1):5862
Zhang T P, Liu L Z, Jia Y H. Test technology of hollow cathode products for electric propulsion system[J].Journal of Rocket Propulsion, 2010,36(1):5862
[17]郭宁,江豪成,顾左. 离子发动机空心阴极寿命预测[J].真空,2009,46(4):8385
Guo N, Jiang H C, Gu Z. Life forecast of hollow cathode for ion engine[J]. Vacuum, 2009,46(4):8385
[18]Ismat M,Rudwan A, Wallace N C, et al. Emitter depletion measurement and modeling in the T5&T6 Kaufmantype ion thrusters[R].IEPC2007256, 2007
[19]贾艳辉,张天平. LIPS200离子推力器工作寿命的分析与验证 [C]. 卫星系统推进技术研讨会,银川,2012
Jia Y H, Zhang T P. Analysis and evaluation of LIPS200 ion thruster operation life[C]. Propulsion Technology of Satellite System Conference, Yinchuan, 2012 |