Evaluation of thermal-deformation reduction method through prototyping space antenna's shape control mechanisms-Reference-Cited by-同舟云学术

Evaluation of thermal-deformation reduction method through prototyping space antenna's shape control mechanisms

Published:2018 Issue:863 Volume:84 Page:17-00566-17-00566
ISSN:2187-9761
Container-title:Transactions of the JSME (in Japanese)
language:en
Short-container-title:

Author:

KASHIYAMA Reo¹,SAKAMOTO Hiraku¹,TANAKA Hiroaki²,OKUMA Masaaki¹,ISHIMURA Kosei³

Affiliation:

1. Tokyo Institute of Technology

2. National Defense Academy of Japan

3. Japan Aerospace Exploration Agency

Publisher

Japan Society of Mechanical Engineers

Link

https://www.jstage.jst.go.jp/article/transjsme/84/863/84_17-00566/_pdf

Reference15 articles.

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2. Bradford, S., Agnes, G., Ohara, C., Green, J., Shi, F., Zhou, H., Peterson, L. and Wilkie, W., Controlling wavefront in lightweight reflector systems using piezocomposite actuator arrays, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA Paper 2013-1525 (2013).

3. Clarricoats, P. J. and Zhou, H., Design and performance of a reconfigurable mesh reflector antenna, IEE Proceedings H, Vol. 138, No. 6 (1991), pp.485-496.

4. Datashvili, L., Baier, H., Wei, B., Hoffman, J., Wehrle, E., Schreider, L., Mangenot, C., Santiage-Prowald, J., Scolamiero, L. and Angevain, J., Mechanical investigations of in-space-reconfigurable reflecting surfaces, 32nd ESA Antenna Workshop on Antennas for Space Applications (2010), pp.1-8.

5. Datashvili, L. S., Baier, H., Wei, B., Endler, S. and Schreider, L., Design of a morphing skin using flexible fiber composites for space-reconfigurable reflectors, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA 2013-1522 (2013).