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Volumn 14, Issue 8, 1977, Pages 461-468

A doubly charged ion model for ion thrusters

Author keywords

Electric and advanced space propulsion

Indexed keywords

ROCKET ENGINES;

EID: 0017526990     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.57224     Document Type: Article
Times cited : (5)

References (14)
  • 10
    • 85003238645 scopus 로고
    • Numerical Procedure for Analyzing Langmuir Probe Data
    • July
    • Beattie, J.R., "Numerical Procedure for Analyzing Langmuir Probe Data," AIAA Journal, Vol. 13, July 1975, pp. 950-952.
    • (1975) AIAA Journal , vol.13 , pp. 950-952
    • Beattie, J.R.1
  • 12
    • 0016225223 scopus 로고
    • Technology of Electron Bombardment Ion Thrusters
    • edited by L. Marton, Academic Press, New York
    • Kaufman, H.R., "Technology of Electron Bombardment Ion Thrusters," Advances in Electronics and Electron Physics, Vol. 36, edited by L. Marton, Academic Press, New York, 1974, pp. 265-373.
    • (1974) Advances in Electronics and Electron Physics , vol.36 , pp. 265-373
    • Kaufman, H.R.1
  • 13
    • 85007695567 scopus 로고
    • Plasma Properties and Performance of Mercury Ion Thrusters
    • Feb
    • Masek, T.D., "Plasma Properties and Performance of Mercury Ion Thrusters," AIAA Journal, Vol. 9, Feb. 1971, pp. 205-212.
    • (1971) AIAA Journal , vol.9 , pp. 205-212
    • Masek, T.D.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.