The proceedings of the JSME annual meeting
Online ISSN : 2433-1325
2005.2
Session ID : 218
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218 Application of a Miniature Rotary-wing Vehicle to Mars Exploration : Its Feasibility and Aerodynamic Characteristics of the Rotor
Noriaki TSUZUKI, Shunichi SATO, Takashi ABE
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Keywords: Miniature Rotorcraft, Mars, Vehicle Density, Flight Robustness, Ultra-low Reynolds Number, Dragonfly
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Abstract

The feasibility and design plans of a miniature rotorcraft for Mars exploration were studied from the standpoint of the aerodynamic characteristics of the rotor at the insect-scale low Reynolds number.

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© 2005 The Japan Society of Mechanical Engineers
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