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Volumn 58, Issue 7-8, 2005, Pages 268-278

Concepts for near-earth asteroid deflection using spacecraft with advanced nuclear and solar electric propulsion systems

Author keywords

Deflection; Impact mitigation; Near Earth asteroids; Nuclear and solar electric propulsion

Indexed keywords

ASTEROID DETECTION; IMPACT MITIGATION; NEAR EARTH ASTERIODS; NUCLEAR AND SOLAR ELECTRIC PROPULSION;

EID: 20744443965     PISSN: 0007084X     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (22)

References (22)
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  • 2
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  • 4
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    • (2004) COSPAR 2004
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  • 5
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    • Deflection techniques: What makes sense?
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    • Harris, A.W.1
  • 6
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  • 7
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  • 8
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    • Close proximity operations for implementing mitigation strategies
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    • D. J. Scheeres, "Close Proximity Operations for Implementing Mitigation Strategies", paper AIAA 2004-1445, 2004 Planetary Defense Conference, Orange County, California, USA, 23-26 February 2004.
    • (2004) Paper AIAA , vol.2004 , Issue.1445
    • Scheeres, D.J.1
  • 9
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    • The B612 mission design
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    • B.G. Williams, D.D. Durda, D.J. Scheeres, "The B612 Mission Design", paper AIAA 2004-1448, 2004 Planetary Defense Conference, Orange County, California, USA, 23-26 February 2004.
    • (2004) Paper AIAA , vol.2004 , Issue.1448
    • Williams, B.G.1    Durda, D.D.2    Scheeres, D.J.3
  • 12
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  • 13
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  • 15
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    • The mechanics of moving asteroids
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    • Scheeres, D.J.1    Schweickart, R.L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.