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Volumn 39, Issue 6, 2002, Pages 933-935

Payload mass fraction optimization for solar sail cargo missions

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; MASS TRANSFER; NUMERICAL METHODS; OPTIMIZATION; ORBITS; PLANETS; SOLAR EQUIPMENT; SOLAR RADIATION; SPACECRAFT PROPULSION; TRAJECTORIES;

EID: 0036872292     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3901     Document Type: Article
Times cited : (6)

References (5)
  • 1
    • 0001563472 scopus 로고
    • An expedition to Mars employing shuttle-era systems, solar sail and aerocapture
    • July-Aug.
    • Staehle, R. L., "An Expedition to Mars Employing Shuttle-Era Systems, Solar Sail and Aerocapture," Journal of the British Interplanetary Society, Vol. 35, July-Aug. 1982, pp. 327-335.
    • (1982) Journal of the British Interplanetary Society , vol.35 , pp. 327-335
    • Staehle, R.L.1
  • 3
    • 84997208337 scopus 로고
    • Space station options for constructing advanced solar sails capable of multiple Mars missions
    • AIAA Paper 87-1902, June
    • Garvey, J. M., "Space Station Options for Constructing Advanced Solar Sails Capable of Multiple Mars Missions," AIAA Paper 87-1902, June 1987.
    • (1987)
    • Garvey, J.M.1
  • 5
    • 85036710781 scopus 로고    scopus 로고
    • Solar sail hybrid trajectory optimisation
    • American Astronautical Society, Paper AAS 01-470, Aug.
    • Hughes, G. W., and McInnes, C. R., "Solar Sail Hybrid Trajectory Optimisation," American Astronautical Society, Paper AAS 01-470, Aug. 2001.
    • (2001)
    • Hughes, G.W.1    McInnes, C.R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.