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Volumn 46, Issue 2, 2009, Pages 340-352

Supersonic inflatable aerodynamic decelerators for use on future robotic missions to mars

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DRAG; DECELERATION; ROBOTICS; SUPERSONIC AIRCRAFT;

EID: 65949120535     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.38562     Document Type: Article
Times cited : (58)

References (22)
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  • 3
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    • Aerodynamic Decelerators for Planetary Exploration: Past, Present, and Future
    • AIAA Paper 2006-6792, Aug
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    • (2006)
    • Cruz, J.R.1    Lingard, J.S.2
  • 5
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    • A Tension Shell Structure for Application to Entry Vehicles
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    • (1965) NASA TN , vol.D-2675
    • Anderson, M.S.1    Robinson, J.C.2    Bush, H.G.3    Fralich, R.W.4
  • 8
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    • A Concept for NASA's Mars 2016 Astrobiology Field Laboratory
    • doi:10.1089/ast.2007. 0153
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    • (2007) Astrobiology , vol.7 , Issue.4 , pp. 545-577
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  • 10
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    • Optimization of Inflatable Drag Devices by Isotensoid Design
    • AIAA Paper 64-437, July
    • Houtz, N. E., "Optimization of Inflatable Drag Devices by Isotensoid Design," AIAA Paper 64-437, July 1964.
    • (1964)
    • Houtz, N.E.1
  • 11
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    • Development Status of Attached Inflatable Decelerators
    • June, doi:10.2514/3.29636
    • Mikulas, M. M., Jr., and Bohon, H. L., "Development Status of Attached Inflatable Decelerators," Journal of Spacecraft and Rockets, Vol. 6, No. 6, June 1969, pp. 654-660. doi:10.2514/3.29636
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  • 13
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    • Aerodynamic Characteristics of Tension Shell Shapes at Mach 3.0
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  • 17
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    • Buckling of a Pressurized Toroidal Ring Under Uniform External Loading
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  • 19
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.