Development of a Low-Density Wind Tunnel for Simulating Martian Atmospheric Flight

Author:

ANYOJI Masayuki1,NOSE Kei1,IDA Shingo1,NUMATA Daiju1,NAGAI Hiroki1,ASAI Keisuke1

Affiliation:

1. Department of Aerospace Engineering, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Reference14 articles.

1. 1)Guynn, M. D, Croom, M. A., Smith, S. C., Parks, R.W, Gelhausen, P.A.: Evolution of a Mars Airplane Concept for the ARES Mars Scout Mission, AIAA Paper 2003-6578, 2003.

2. 2)Braun, R. D. and Spencer, D. A.: Design of the ARES Mars Airplane and Mission Architecture, J. Spacecraft and Rockets, 43 (2006), pp. 1026-1034.

3. 3)Rinoie, K.: Mars Airplane for Geographical Exploration –Conceptual Design Results from Student Design Projects, The 2nd International Symposium on Innovative Aerial/Space Flyer Systems, Tokyo, Dec. 2-3, 2005.

4. 4)Oyama, A. and Fuji, K.: A Study on Airfoil Design for Future Mars Airplane, AIAA Paper 2006-1484, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 9-12, 2006.

5. 5)McMasters, J. H. and Henderson, M. L.: Low Speed Single Element Airfoil Synthesis, Technical Soaring, 6 (1980), pp. 1-21.

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