A Feasibility Analysis of Collaborative Mission Using Mars Airplane and Mars Balloon - Mars Aerial-Exploration for Terrestrial and Tropospheric Environment Observation -

Author:

TANAKA Hiroto12,MAMIYA Issei12,KIRITANI Hideki12,NAGASAWA Hiroki12,HIRATA Takumi12,TONAI Tatsuya12,NAGAI Hiroki1,FUJITA Koji1

Affiliation:

1. Institute of Fluid Science, Tohoku University

2. Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Reference26 articles.

1. 1) Hassanalian, M., Rice, D., and Adbelkefi, A.: Evolution of Space Drones for Planetary Exploration: A review. Progress in Aerospace Sciences, 97 (2018), pp. 61–105.

2. 2) Braun, R. D., 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. 4) Fujita, K., Nagai, H., and Oyama, A.: AParametric Study of Mars Airplane Concept for Science Mission on Mars, Trans. JSASS Aerospace Tech Japan, 14, ists30(2016), pp. Pk_83–Pk_88.

4. 5) Goto, Y., Kaku, T., Haruyama, J., and Miyake, W.: List of Hole Pits taken by MRO HiRISE at the foot of Elysium Mons on Mars, JAXA-RM-16-008, 2017 (in Japanese).

5. 6) Shigeoka, S., Ochi, H., Yonemoto, K.: About Aspect Ratio Study on Three Dimensional Wing at Low Reynolds Number Flow Using Variable-Pressure Wind Tunnel, Proc. Of the 64th Kyushu Branch Regular Meeting of the JSME, Fukuoka, C42, 2011 (in Japanese).

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