Overall Achievements of the Flight Demonstration of EGG: Re-entry Nano-Satellite with Gossamer Aeroshell and GPS/Iridium-Reference-Cited by-同舟云学术

Overall Achievements of the Flight Demonstration of EGG: Re-entry Nano-Satellite with Gossamer Aeroshell and GPS/Iridium

Published:2024 Issue:4 Volume:67 Page:224-233
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

YAMADA Kazuhiko¹,MORIYOSHI Takahiro¹²,MATSUMARU Kazushige³,KANEMARU Hiroki²,ARAYA Takahiro⁴,SUZUKI Kojiro⁵,IMAMURA Osamu³,AKITA Daisuke⁶,NAGATA Yasunori¹⁷,WATANABE Yasumasa⁸⁹

Affiliation:

1. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

2. Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology

3. College of Industrial Technology, Nihon University

4. Department of Material Science and Technology, Tokyo University of Science

5. Graduate School of Frontier Sciences, The University of Tokyo

6. Department of International Development Engineering, Tokyo Institute of Technology

7. Graduate School of Natural Science and Technology, Okayama University

8. Department of Aeronautics and Astronautics, The University of Tokyo

9. School of Engineering, Toyota Technological Institute

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tjsass/67/4/67_T-22-56/_pdf

Reference22 articles.

1. 1) Rohrschneider, R. R. and Braun, R. D.: Survey of Ballute Technology for Aerocapture, J. Spacecraft Rockets, 44, 1 (2007), pp. 10–23. doi: 10.2514/1.19288

2. 2) Gräßilin, M. and Schöttle, U.: Flight Performance Evaluation of the Re-entry Mission IRDT-1, International Aeronautical Federation Paper IAF-01-v.3.05, Oct. 2001.

3. 3) Hughes, S., Dillman, R., Starr, B., Stephan, R., Lindell, M., Player, C., and Cheatwood, F.: Inflatable Re-entry Vehicle Experiment (IRVE) Design Overview, 18th AIAA Aerodynamic Decelerator Systems Technology Conference, AIAA 2005-1636, 2005.

4. 4) Hughes, S., Cheatwood, F., Dillman, R., Calomino, A., Wright, H., DelCorso, J., and Calomino, A.: Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Technology Development Overview, 21st AIAA Aerodynamic Decelerator Systems Technology Conference, AIAA 2011-2524, 2011.

5. 5) Venkatapathy, E., Hamm, K., Fernandez, I., Arnold, J., Kinney, D., Laub, B., Makino, A., McGuire, M., Peterson, K., Prabhu, D., Empey, D., Dupzyk, I., Huynh, L., Hajela, P., Gage, P., Howard, A., and Andrews, D.: Adaptive Deployable Entry and Placement Technology (ADEPT): A Feasibility Study for Human Missions to Mars, 21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, AIAA-2011-2608, 2011.