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Volumn 120, Issue II, 2005, Pages 1875-1901

Trajectories leaving a sphere in the restricted 3-body problem

Author keywords

[No Author keywords available]

Indexed keywords

GALILEAN SATELLITES; JACOBI CONSTANT; JUPITER;

EID: 26944440400     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (14)

References (11)
  • 1
    • 0000883588 scopus 로고
    • Low energy transit orbits in the restricted three-body problem
    • Conley, C., "Low energy transit orbits in the restricted three-body problem", SIAM Journal of Applied Mathematics, Vol. 61, pp. 732-746, 1968.
    • (1968) SIAM Journal of Applied Mathematics , vol.61 , pp. 732-746
    • Conley, C.1
  • 2
    • 0016561173 scopus 로고
    • Jupiter orbiter lifetime - Hazard of galilean satellite collision
    • Friedlander, A.L., "Jupiter Orbiter Lifetime - Hazard of Galilean Satellite Collision", Journal of the Astronautical Sciences, Vol. 23, No. 4, pp. 349-368, 1995.
    • (1995) Journal of the Astronautical Sciences , vol.23 , Issue.4 , pp. 349-368
    • Friedlander, A.L.1
  • 4
    • 0031109096 scopus 로고    scopus 로고
    • Application of dynamical systems theory to trajectory design for a libration point
    • April-June
    • Howell, K., Barden, B., Lo, M., "Application of Dynamical Systems Theory to Trajectory Design for a Libration Point", Journal of the Astronautical Sciences, Vol. 45, No. 2, April-June 1997.
    • (1997) Journal of the Astronautical Sciences , vol.45 , Issue.2
    • Howell, K.1    Barden, B.2    Lo, M.3
  • 5
    • 84888891890 scopus 로고    scopus 로고
    • Paper No. 98-4468, AIAA/AAS Astrodynamics Conference, Boston, MA, August
    • Lo M.W., et al., Genesis Mission Design, Paper No. 98-4468, AIAA/AAS Astrodynamics Conference, Boston, MA, August, 1998.
    • (1998) Genesis Mission Design
    • Lo, M.W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.