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Volumn , Issue , 2003, Pages

Status of the extended life test of the deep space 1 flight spare ion engine after 30,352 hours of operation

Author keywords

[No Author keywords available]

Indexed keywords

DISCHARGE CATHODE KEEPERS; ELECTRICAL ISOLATION; ENGINE DEVELOPMENT; OPERATIONAL CHARACTERISTICS; PERFORMANCE DEGRADATION; POST-TEST ANALYSIS; THRUSTER PERFORMANCE; XENON PROPELLANT;

EID: 84897586017     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (66)

References (26)
  • 1
    • 18844365505 scopus 로고    scopus 로고
    • Demonstration of the NSTAR Ion Propulsion System on the Deep Space One Mission
    • October
    • Polk, J. E., et al, "Demonstration of the NSTAR Ion Propulsion System on the Deep Space One Mission, " 27th International Electric Propulsion Conference, October 2001.
    • (2001) 27th International Electric Propulsion Conference
    • Polk, J.E.1
  • 3
    • 69249125633 scopus 로고    scopus 로고
    • In-Flight Performance of the NSTAR Ion Propulsion System on the Deep Space One Mission
    • March
    • Polk, J. E., et al., "In-Flight Performance of the NSTAR Ion Propulsion System on the Deep Space One Mission, " Z8_0304. PDF, IEEE Aerospace Conference Proceedings, March 2000.
    • (2000) Z8_0304. PDF, IEEE Aerospace Conference Proceedings
    • Polk, J.E.1
  • 10
    • 84897788357 scopus 로고    scopus 로고
    • Performance Characteristics of the NSTAR Ion Thruster During an On-Going Long Duration Ground Test
    • March
    • Anderson, J. R., et al., "Performance Characteristics of the NSTAR Ion Thruster During an On-Going Long Duration Ground Test, " Z8_0303. PDF, IEEE Aerospace Conference Proceedings, March 2000.
    • (2000) Z8_0303. PDF, IEEE Aerospace Conference Proceedings
    • Anderson, J.R.1
  • 17


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.