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Volumn 886, Issue , 2007, Pages 303-316

Comparison of single and multi-spacecraft configurations for NEA deflection by solar sublimation

Author keywords

Asteroid deflection method; Near Earth Object; Solar sublimation; Spacecraft formation flying

Indexed keywords


EID: 33947361568     PISSN: 0094243X     EISSN: 15517616     Source Type: Conference Proceeding    
DOI: 10.1063/1.2710064     Document Type: Conference Paper
Times cited : (25)

References (15)
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    • 33746563780 scopus 로고    scopus 로고
    • Optimal interception and deflection of Earth-approaching asteroids using low-thrust electric propulsion
    • Cambridge University Press, Cambridge, UK
    • Conway B., "Optimal interception and deflection of Earth-approaching asteroids using low-thrust electric propulsion" in Mitigation of hazardous comets and asteroids, Cambridge University Press, Cambridge, UK (2004).
    • (2004) Mitigation of hazardous comets and asteroids
    • Conway, B.1
  • 7
    • 33947386320 scopus 로고    scopus 로고
    • Wertz, J. R, and Larson, W. J, Eds, 3rd Ed, Microcosm Press & Kluwer Academic Publishers, California
    • rd Ed., Microcosm Press & Kluwer Academic Publishers, California, 1999.
    • (1999) Space Mission Analysis and Design
  • 9
  • 15


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.