This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Preliminary Design of JEM Environmental Control and Life Support System
Annotation ability available
Sector:
Language:
English
Abstract
This paper outlines the current status of the preliminary design study of the Japanese Experimental Module (JEM) Environmental Control and Life Support System (ECLSS), one of the subsystems in JEM which is attached to the Space Station core.
ECLSS functions to be provided are defined and identified based on the system requirements levied on JEM ECLSS.
The design concepts for ECLSS function allocation between JEM and the SS core, and JEM ECLSS function/hardware distribution are also established.
In addition, the issues and concerns related to the ECLSS interface between the SS core and JEM are introduced.
The design approach emphasizes the JEM emergency system concept with respect to contamination control and monitoring and to fire detection and suppression, which must be standardized throughout all modules in SS.
Authors
Topic
Citation
Shiraki, K., Hashimoto, H., Manabe, K., Hattori, A. et al., "Preliminary Design of JEM Environmental Control and Life Support System," SAE Technical Paper 891574, 1989, https://doi.org/10.4271/891574.Also In
References
- JEM System Specifications NASDA-ESPC-840 February 28 1989
- Space Station Program Definition and Requirements NASA, SSP 30000 Sec.3, Rev.G October 31 1988
- Architectural Control Document, Environmental Control and Life Support System NASA, SSP 30262, Rev.B July 30 1988
- 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, L-3-5 May 1988