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Volumn 120, Issue II, 2005, Pages 1185-1204

Trajectory design and maneuver strategy for the MESSENGER mission to Mercury

Author keywords

[No Author keywords available]

Indexed keywords

COMPLEX MISSION PLAN; TRAJECTORY ADJUSTMENTS; TRAJECTORY DESIGN;

EID: 26944461141     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (13)
  • 4
    • 0035729165 scopus 로고    scopus 로고
    • New trajectory options for ballistic Mercury orbiter mission
    • Spaceflight Mechanics 2001
    • Yen, C. L., "New Trajectory Options for Ballistic Mercury Orbiter Mission," Spaceflight Mechanics 2001, Advances in the Astronautical Sciences, 108, Part II, 799-806, 2001.
    • (2001) Advances in the Astronautical Sciences , vol.108 , Issue.2 PART , pp. 799-806
    • Yen, C.L.1
  • 5
    • 84983201976 scopus 로고    scopus 로고
    • Discovery class Mercury orbiter trajectory design for the 2005 launch opportunity
    • AIAA-98-4283, Boston, MA, August 10-12
    • McAdams, J. V., J. L. Horsewood, and C. L. Yen, "Discovery Class Mercury Orbiter Trajectory Design for the 2005 Launch Opportunity," AIAA-98-4283, 7 pp., AIAA/AAS Astrodynamics Specialist Conference, Boston, MA, August 10-12, 1998.
    • (1998) AIAA/AAS Astrodynamics Specialist Conference
    • McAdams, J.V.1    Horsewood, J.L.2    Yen, C.L.3
  • 6
    • 0034223701 scopus 로고    scopus 로고
    • Chemical and solar electric propulsion options for a mercury cornerstone mission
    • Langevin, Y., "Chemical and Solar Electric Propulsion Options for a Mercury Cornerstone Mission," Acta Astronautica, 47, No. 2-9, 443-452, 2000.
    • (2000) Acta Astronautica , vol.47 , Issue.2-9 , pp. 443-452
    • Langevin, Y.1
  • 7
    • 0008794181 scopus 로고    scopus 로고
    • A resilient mission design for the MESSENGER 2004 Mercury orbiter
    • AIAA-99-IAA. 11.2.06, Amsterdam, The Netherlands, October 4-8
    • th International Astronautical Congress, Amsterdam, The Netherlands, October 4-8, 1999.
    • (1999) th International Astronautical Congress
    • McAdams, J.V.1
  • 8
    • 0036069103 scopus 로고    scopus 로고
    • Improvements in trajectory optimization for MESSENGER: The first Mercury orbiter mission,"
    • Astrodynamics 2001
    • McAdams, J. V., R. W. Farquhar, and C. L. Yen, "Improvements in Trajectory Optimization for MESSENGER: The First Mercury Orbiter Mission," Astrodynamics 2001, Advances in the Astronautical Sciences, 109, Part III, 2189-2203, 2002.
    • (2002) Advances in the Astronautical Sciences , vol.109 , Issue.3 PART , pp. 2189-2203
    • McAdams, J.V.1    Farquhar, R.W.2    Yen, C.L.3
  • 9
    • 1542269797 scopus 로고    scopus 로고
    • MESSENGER Mercury orbiter trajectory design
    • Spaceflight Mechanics 2003
    • McAdams, J. V., "MESSENGER Mercury Orbiter Trajectory Design," Spaceflight Mechanics 2003, Advances in the Astronautical Sciences, 114, Part III, 1549-1567, 2003.
    • (2003) Advances in the Astronautical Sciences , vol.114 , Issue.3 PART , pp. 1549-1567
    • McAdams, J.V.1
  • 11
    • 85086615998 scopus 로고    scopus 로고
    • Design and development of the MESSENGER propulsion system
    • Paper AIAA-2003-5078, Huntsville, AL, July 21-24
    • Wiley, S., K. Dommer, and L. Mosher, "Design and Development of the MESSENGER Propulsion System," AIAA/SAE/ASME Joint Propulsion Conference, Paper AIAA-2003-5078, 20 pp., Huntsville, AL, July 21-24, 2003.
    • (2003) AIAA/SAE/ASME Joint Propulsion Conference
    • Wiley, S.1    Dommer, K.2    Mosher, L.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.