System Design, Development and Ground Verification of a Separable De-Orbit Mechanism for the Orbital Manoeuvre of Micro-Satellite ALE-1-Reference-Cited by-同舟云学术

System Design, Development and Ground Verification of a Separable De-Orbit Mechanism for the Orbital Manoeuvre of Micro-Satellite ALE-1

Published:2021 Issue:3 Volume:19 Page:360-367
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

PALA Alperen¹,KUWAHARA Toshinori¹,HONDA Tomoyuki¹,UTO Hiroki²,KANEKO Tetsuya²,POTIER Adrien¹,TANGDHANAKANOND Pasith¹,FUJITA Shinya¹,SHIBUYA Yoshihiko¹,SATO Yuji¹,SHIBUYA Tomomasa¹,KAMACHI Koh³

Affiliation:

1. Department of Aerospace Engineering, Tohoku University

2. Nakashimada Engineering Works, Ltd.

3. ALE Co., Ltd.

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/19/3/19_19.360/_pdf

Reference23 articles.

1. 1) Kuwahara, T., Fujita, S., Sato, Y., Shibuya, Y., Pala, A., Kamachi, K., and Okajima, L.: ALE Satellite Project, Proceeding of 61st Space Sciences and Technology Conference, Kurume, Japan, JSASS2018-4010, 2018 (in Japanese).

2. 2) Myers, R. M., Oleson, S. R., Curran, F. M., and Schneider, S. J.: Small Satellite Propulsion Options, 30th Joint Propulsion Conference, Indianapolis, Indiana, 1994.

3. 3) Innovative Satellite Technology Demonstration Program, http://www.kenkai.jaxa.jp/eng/research/innovative/innovative.html (accessed April 4, 2019).

4. 4) Hoyt, R. P., Barnes, I. M., Voronka, N. R., and Slostad, J. T.: The Terminator Tape™: A Cost-Effective De-Orbit Module for End-of Life Disposal of LEO Satellites, AIAA Paper 2009-6733, 2009.

5. 5) Roberts, P. C. E. and Harkness, P. G.: Drag Sail for End-of-life Disposal from Low Earth Orbit, J. Spacecraft and Rockets, 44 (2007), pp. 1195–1203.

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