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Volumn , Issue , 2003, Pages

Performance Evaluation of the Next Ion Engine

Author keywords

[No Author keywords available]

Indexed keywords

DISCHARGE CHAMBER; ENGINE INLETS; GRID SERVICES; INLET PRESSURES; OPERATING TEMPERATURE RANGES; PERFORMANCE TESTS; SPECIFIC IMPULSE; THRUST EFFICIENCY;

EID: 84897585746     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (33)

References (14)
  • 1
    • 0034432352 scopus 로고    scopus 로고
    • In-Flight Performance of the NSTAR Ion Propulsion System on the Deep Space One Mission
    • Paper 8.0304, March
    • Polk, J.E., et al., "In-Flight Performance of the NSTAR Ion Propulsion System on the Deep Space One Mission, " IEEE Aerospace Conference Paper 8.0304, March 2000.
    • (2000) IEEE Aerospace Conference
    • Polk, J.E.1
  • 11
    • 0021494011 scopus 로고
    • Improved Ion Containment Using a Ring-Cusp Ion Thruster
    • September-October
    • Sovey, J.S., "Improved Ion Containment Using a Ring-Cusp Ion Thruster, " Journal of Spacecraft and Rockets, vol. 21, no. 5, September-October 1984, p. 489.
    • (1984) Journal of Spacecraft and Rockets , vol.21 , Issue.5 , pp. 489
    • Sovey, J.S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.