Superplastic Titanium Tanks for Propulsion System of Satellites

Author:

Sato Eiichi1,Sawai S.1,Uesugi K.1,Takami T.2,Furukawa K.2,Kamada M.2,Kondo M.3

Affiliation:

1. Japan Aerospace Exploration Agency

2. Mitsubishi Heavy Industries Ltd.

3. Muroran Institute of Technology

Abstract

Institute of Space and Astronautical Science (ISAS/JAXA) in collaboration with Mitsubishi Heavy Industries (MHI) has developed fuel and gas tanks for reaction control system and orbital control system of satellites; A tank is fabricated through welding of two thin, hemi-spherical or conical parts, which are fabricated by superplastic blow forming. Mass-productivity is not an important factor but the forming precision and flexibiliry in the process are important for this application. ISAS and MHI, therefore, developed a new blow-forming technique, which has high flexibility in terms of tank size because it requires a furnace but not a hot-press machine. Some typical propulsion tanks fabricated through this process are presented.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference4 articles.

1. K. Furukawa, T. Fujita, A. Yamada and M. Nagatomo: Mistubishi Heavy Industries, Ltd. Technical Review Vol. 34(1997), p.30.

2. S. Nakajima, Mistubishi Heavy Industries, Ltd. Technical Review Vol. 39 (2002), p.55.

3. A. Takahashi, S. Shimizu and T. Tsuzuku: J. of the JSTP Vol. 31 (1990), p.1128.

4. E. Sato, T. Yamada, H. Tanaka and I. Jimbo: Mater. Trans. Vol. 47 (2006) p.1121.

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