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Volumn , Issue , 2003, Pages

A preliminary 2-D computational model of an ion thruster discharge chamber

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL MESH; COMPUTATIONAL MODEL; DESIGN AND OPTIMIZATION; EMPIRICAL INVESTIGATION; MAGNETIC CHANNELS; MAGNETIC POTENTIALS; THERMAL TRANSPORT; TWO DIMENSIONAL MODEL;

EID: 84897788164     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (16)
  • 6
    • 0022160724 scopus 로고
    • Simple Performance Model for Ring and Line Cusp Ion Thrusters
    • Brophy J., Wilbur P., "Simple Performance Model for Ring and Line Cusp Ion Thrusters, " AIAA Journal, Vol. 23, pp. 1731-1736, 1985.
    • (1985) AIAA Journal , vol.23 , pp. 1731-1736
    • Brophy, J.1    Wilbur, P.2
  • 8
    • 0000365141 scopus 로고
    • Ion Source Discharge Performance and Stability
    • June
    • Goebel D., "Ion Source Discharge Performance and Stability, " Phys. Fluids 25(6), June 1982.
    • (1982) Phys. Fluids , vol.25 , Issue.6
    • Goebel, D.1
  • 9
  • 12
    • 0000948925 scopus 로고    scopus 로고
    • The Flow of Highly Rarefied Gases Through Tubes of Arbitrary Length
    • Clausing P., "The Flow of Highly Rarefied Gases Through Tubes of Arbitrary Length, " Journal of Vacuum Science and Technology, Vol. 8, No. 5.
    • Journal of Vacuum Science and Technology , vol.8 , Issue.5
    • Clausing, P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.