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Structure Design Considerations of Engineering Test Satellite VI as Large Geostationary Satellite Bus
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English
Abstract
This paper presents the results of some structural design considerations on Japanese Engineering Test Satellite VI (ETS-VI) as Large Geostationary Satellite Bus for the application satellites in the 1990's. And further the structural system development planning is discussed.
Citation
Mitsuma, H., "Structure Design Considerations of Engineering Test Satellite VI as Large Geostationary Satellite Bus," SAE Technical Paper 872431, 1987, https://doi.org/10.4271/872431.Also In
References
- Mitsuma H. “Structural concept of Japanese advanced geostationary spacecraft,” Proceedings of a conference: “Spacecraft Structures,” CNES Toulouse 3-6 December 1985 April 1986 255 260
- Mitsuma H. Yamamoto M. Nakamaru K. Okuda K. Imai R. “Structural Design and Component Tests of Large Geostationary Satellite Bus,” Proceedings of the fifteenth International Symposium on Space Technology and Science Tokyo 1986 455 464
- Mitsuma H. Imai R. Suzuki H. Kawashima J. Ido Y. Ishibashi T. Kuriyama Y. “Development of Light Weight Payload Radiator with Heat Pipes for a 2-ton Geostationary Satellite,” Sixth International Heat Pipe Conference Grenoble, France May 25-28 1987
- Mitsuma H. “Technical issues in environmental test and evaluation of spacecraft structures,” Proceedings of 4th International Conference on Structural Safety and Reliability Kobe, Japan 1985 III III-585 III-590