High-Speed Aerodynamic Characteristics of a Deployable-Wing Airplane for Mars Exploration
Author:
Affiliation:
1. Department of Mechanical Engineering, Tokai University
2. Department of Mechanical and Aerospace Engineering, Tottori University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/astj/15/0/15_JSASS-D-15-00055/_pdf
Reference8 articles.
1. 1) Guynn, M. D., Croom, M. A., Smith, S. C., Parks, R. W. and Gelhausen, P. A.: Evolution of a Mars Airplane Concept for the ARES Mars Scout Mission, AIAA Paper 2003-6578, 2003.
2. 2) Braun, R., Wright, H. S., Croom, M. A., Levine, J. S. and Spencer, D. A.: Design of the ARES Mars Airplane and Mission Architecture, J. Spacecraft and Rockets, 43 (2006), pp. 1026-1034.
3. 3) Oyama, A. and Fujii, K.: A Study on Airfoil Design for Future Mars Airplane, AIAA Paper 2006-1484, 2006.
4. 4) Fujita, K., Luong, R., Nagai, H. and Asai, K.: Conceptual Design of Mars Airplane, Transactions of JSASS, Aerospace Technology Japan, 10, ists28 (2012), pp. Te_5-Te_10.
5. 5) Anyoji, M., Okamoto, M., Hidaka, H., Nonomura, T., Oyama, A., and Fujii, K.: Planetary Atmosphere Wind Tunnel Tests on Aerodynamic Characteristics of a Mars Airplane Scale Model, Transactions of JSASS, Aerospace Technology Japan, 12, ists29 (2014), pp. Pk_7-Pk_12.
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