[1]Jacobson D T, John J, Kamhawi H, et al. An Overview of Hall Thruster Development at NASA's John H. Glenn Research Center[R]. AIAA 2005-4242. [2]Van-Noord J L, Kamhawi H, Mcewen H K. Characterization of a High Current, Long Life Hollow Cathode[R]. NASA/TM 2006-214095. [3]Randolph T, Polk J. An Overview of the Nuclear Electric Xenon Ion System (NEXIS) Activity [R]. AIAA 2004-3450. [4]Rovey J L, Gallimore A D. Dormant Cathode Plasma Properties and Erosion Analysis in a Multiple-Cathode, High-Power, Rectangular Discharge Chamber[R]. AIAA 2005-4241. [5]张天平. 国外电推进系统空心阴极技术现状[J]. 上海航天, 2008, 25(1): 39-46. [6]Polk J E, Kakuda R Y, Brinza D, et al. Demonstration of the NSTAR Ion Propulsion System on the Deep Space One Mission[R]. IEPC 2001-075. [7]Sengupta A, Brophy J R., Goodfellow K D. An Overview of the Results from the 30,000 Hr Life Test of Deep Space 1 Flight Spare Ion Engine[R]. AIAA 2004-3608. [8]Sengupta A. Destructive Physical Analysis of Hollow Cathodes from the Deep Space 1 Flight Spare Ion Engine 30,000 Hr Life Test[R]. IEPC 2005-026. [9]张天平. 电推进系统空心阴极研制试验技术[J]. 真空电子技术, 2007, 12(2): 9-14. [10]Geobel D M, Katz I, Polk J, Mikellides I G. Extending Hollow Cathode Life for Electric Propulsion in Long-Term Missions[R]. AIAA 2004-5911. [11]Tighe W G, Chien K R, Goebel D M, et al. Hollow Cathode Ignition and Life Model[R]. AIAA 2005-3666. [12]Kovaleski S D. Life Model of Hollow Cathodes Using a Barium Calcium Aluminate Impregnated Tungster Emitter[R]. IEPC 2001-276.