메뉴 건너뛰기




Volumn , Issue , 2002, Pages

Performance characteristics of the deep space 1 flight spare ion thruster long duration test after 21,300 hours of operation

Author keywords

[No Author keywords available]

Indexed keywords

DEPOSIT FORMATION; DISCHARGE CATHODE KEEPERS; ELECTRICAL ISOLATION; IDENTIFICATION OF UNKNOWNS; JET PROPULSION LABORATORY; PERFORMANCE CHARACTERISTICS; PERFORMANCE DEGRADATION; PRIMARY OBJECTIVE;

EID: 84896693670     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (22)
  • 3
    • 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
  • 5
    • 69249125633 scopus 로고    scopus 로고
    • In-Flight Performance of the NSTAR Ion Propulsion System on the Deep Space One Mission
    • IEEE Aerospace Conference Proceedings, 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
    • Polk, J.E.1
  • 11


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.