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Status of JEM ECLSS Design
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English
Abstract
The preliminary design of the Japanese Experiment Module (JEM) has started in January 1990. As a result of the JEM configuration review activity which was focused on the development cost and schedule prior to getting into the preliminary design, a part of the JEM Environmental Control and Life Support System (ECLSS) functions was changed.
This paper presents the JEM ECLS system baseline and the subsystem configuration at the start of the Phase C/D. Also the outline of the preliminary cabin air ventilation testing which started in March 1989 is described.
Authors
- F. Otsuki - National Space Development Agency of Japan (NASDA)
- T. Suzuki - National Space Development Agency of Japan (NASDA)
- N. Yamaguchi - National Space Development Agency of Japan (NASDA)
- A. Hattori - Kawasaki Heavy Industries, Ltd. (KHI)
- Y. Yoshida - Kawasaki Heavy Industries, Ltd. (KHI)
- H. Iwasaki - Kawasaki Heavy Industries, Ltd. (KHI)
Topic
Citation
Otsuki, F., Suzuki, T., Yamaguchi, N., Hattori, A. et al., "Status of JEM ECLSS Design," SAE Technical Paper 901209, 1990, https://doi.org/10.4271/901209.Also In
References
- JEM System Specifications NASDA-ESPC-840A October 24 1989
- Space Station Program Definition and Requirements NASA SSP 30000 November 30 1989
- Architectural Control Document, Environmental Control and Life Support System NASA SSP 30262
- Environmental Control and Life Support System for Japanese Experimental Module Shiraki K. Fujimori H. Hattori A. ICES/SAE, 871429 July 1987
- JEM Environmental Control and Life Support System Shiraki K. Manabe K. Fujimori H. Hattori A. Hama H. #16 ISTS May 1988
- Preliminary Design of JEM Environmental Control and Life Support System Shiraki K. Hashimoto H. Manabe K. Hattori A. Hama H. ICES/SAE, 891574 July 1989