Improvement of a Shape Accuracy Considering the Characteristics of Cable Network Systems for Large Mesh Antenna Reflectors

Author:

HARADA Satoshi,MEGURO Akira,UEBA Masazumi

Publisher

Japan Society for Aeronautical and Space Sciences

Reference10 articles.

1. 1) Natori, M. C., Inoue, T. and Kitamura, T.: Deployable Mesh Antenna Structure for MUSES-B Spacecraft, IAF-95-I.1.04, Oslo, 1995.

2. 2) Meguro, A., Tsujihata, A., Hamamoto, N. and Honma, M.: Technology Status of the 13m Aperture Deployment Antenna Reflectors for Engineering Test Satellite VIII, IAF-99-I.6.01, Amsterdam, 1999.

3. 3) Meguro, A., Harada, S. and Ueba, M.: Structural Characteristics of an Ultra-Light Large Antenna Reflector Onboard Communication Satellites, 55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, IAC04-I.1.09, Vancouver, 2004.

4. 4) Natori, M. C.: Ground Adjustment Procedure of a Deployable High Accuracy Mesh Antenna for Space VLBI Mission, 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum, Long Beach, CA, AIAA Paper 1998-1923, 1998.

5. 5) Uchimaru, K., Nakamura, K., Tsujihata, A., Miyasaka, A. and Meguro, A.: Large Deployable Reflector on ETS-VIII.II, 18th International Communications Satellite Systems Conference and Exhibit, Technical Papers, Vol. 1, Oakland, AIAA Paper 2000-1144, 2000.

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