The International Space Station (ISS) Environmental Control and Life Support (ECLS) system includes regenerative and non-regenerative technologies which provide the basic life support functions to support the crew, while maintaining a safe and habitable shirt-sleeve environment. Significant progress has been made over the past year including initial assembly flights of the Functional Cargo Block (FGB) and Node 1 modules. The remaining Phase 2 elements have completed significant element integration testing with ECLS hardware deliveries complete, while the Phase 3 elements and regenerative ECLS design activities have continued. This paper provides a summary of the U.S. Environmental Control and Life Support (ECLS) system activities over the past year.
International Space Station Environmental Control and Life Support System Status: 1998-1999
Sae Technical Papers
International Conference On Environmental Systems ; 1999
1999-07-12
Conference paper
English
International Space Station Environment Controland Life Support System Status: 1998-1999
British Library Conference Proceedings | 1999
|International Space Station Environmental Control and Life Support System Status: 1997-1998
British Library Conference Proceedings | 1998
|International Space Station Environmental Control and Life Support System Status: 1997-1998
SAE Technical Papers | 1998
|International Space Station Environmental Control and Life Support System Status: 1999-2000
SAE Technical Papers | 2000
|International Space Station Environmental Control and Life Support System Status: 1999-2000
British Library Conference Proceedings | 2000
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