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Volumn 2, Issue , 2003, Pages 625-635

Analysis and experimentation for the aerial deployment of planetary balloons

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL MODEL; LARGE DISPLACEMENTS; NON-LINEAR FINITE ELEMENT MODEL; PLANETARY BALLOONS; POLYMER BALLOONS; PREDICTIVE ABILITIES; RIGID BODY MODELS; SPRING-MASS MODEL;

EID: 67349206010     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.2003.1235472     Document Type: Conference Paper
Times cited : (11)

References (6)
  • 2
    • 3042583966 scopus 로고    scopus 로고
    • Breakthrough in mars balloon technology
    • Paper PSB1-0076-02, Houston, TX, USA, 10-19 October
    • V. V. Kerzhanovich et al, "Breakthrough in Mars Balloon Technology", Paper PSB1-0076-02, 34th COSPAR Scientific Assembly, Houston, TX, USA, 10-19 October, 2002.
    • (2002) 34th COSPAR Scientific Assembly
    • Kerzhanovich, V.V.1
  • 3
    • 84879367863 scopus 로고    scopus 로고
    • Multibody modeling and dynamics of parachute and balloon flight systems for planetary exploration
    • Paper AIAA 2001-2026, Boston, MA
    • M. Quadrelli, J. Cameron, V. Kerzhanovich, "Multibody Modeling and Dynamics of Parachute and Balloon Flight Systems for Planetary Exploration," Paper AIAA 2001-2026, 16th AIAA Aerodynamics Decelerator Conference, Boston, MA, 2001.
    • (2001) 16th AIAA Aerodynamics Decelerator Conference
    • Quadrelli, M.1    Cameron, J.2    Kerzhanovich, V.3
  • 4
    • 0024656954 scopus 로고    scopus 로고
    • Determining and accounting for parachute virtual mass
    • Yavuz, T., "Determining and Accounting for Parachute Virtual Mass," AIAA Journal of Aircraft, Vol. 26 No. 5. 1989.
    • AIAA Journal of Aircraft , vol.26 , Issue.5 , pp. 1989
    • Yavuz, T.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.