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Volumn , Issue , 2003, Pages

Analytical model of electron backstreaming for ion thrusters

Author keywords

[No Author keywords available]

Indexed keywords

ANALYTIC-AND-NUMERICAL METHODS; ANALYTICAL EQUATIONS; FINITE THICKNESS; GRID VOLTAGE; HIGH SPECIFIC IMPULSE; ION FOCUSING; ION OPTICS DESIGNS; SPACE CHARGE EFFECTS;

EID: 84897818214     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (14)

References (10)
  • 1
    • 0016225223 scopus 로고
    • Technology of Electron-Bombardment Ion Thrusters
    • Academic Press, San Francisco
    • H.R. Kaufman, "Technology of Electron-Bombardment Ion Thrusters", Advances in Electronics and Electron Physics, V. 36, pp. 301-303, Academic Press, San Francisco, 1974.
    • (1974) Advances in Electronics and Electron Physics , vol.36 , pp. 301-303
    • Kaufman, H.R.1
  • 3
    • 0025489121 scopus 로고
    • An Approach to the Parametric Design of Ion Thrusters
    • Sept.-Oct
    • P.J. Wilbur, J.R. Beattie and J. Hyman, Jr., "An Approach to the Parametric Design of Ion Thrusters, " J. Prop. and Power, V. 6, No. 5, Sept.-Oct. 1990, pp. 575-583.
    • (1990) J. Prop. and Power , vol.6 , Issue.5 , pp. 575-583
    • Wilbur, P.J.1    Beattie, J.R.2    Hyman Jr., J.3
  • 7
    • 84896693670 scopus 로고    scopus 로고
    • Performance Characteristics of the Deep Space 1 Flight Spare Ion Thruster Long Duration Test after 21, 300 hrs of Operation
    • Cleveland, OH, Also see references cited by this work
    • A. Sengupta, J.R. Anderson, and J.R. Brophy, K. Rawlin, and J.S. Sovey, "Performance Characteristics of the Deep Space 1 Flight Spare Ion Thruster Long Duration Test after 21, 300 hrs of Operation, " AIAA-01-3959, Joint Propulsion Conference, Cleveland, OH, 2002. Also see references cited by this work.
    • (2002) AIAA-01-3959, Joint Propulsion Conference
    • Sengupta, A.1    Anderson, J.R.2    Brophy, J.R.3    Rawlin, K.4    Sovey, J.S.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.