Potential and benefits of closed loop ECLS systems on the ISS

Acta Astronautica

Volumn 48, Issue 5-12, 2001, Pages 411-419

  Raatschen, Willigert ^a   Preiss, Helmut ^a  

^a AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTROCHEMISTRY; ELECTROLYSIS; FUEL CELLS; MANNED SPACE FLIGHT; SPACECRAFT POWER SUPPLIES;

ATTITUDE CONTROL;

LIFE SUPPORT SYSTEMS (SPACECRAFT);

CARBON DIOXIDE; OXYGEN; ZEOLITE;

AIR CONDITIONING; ARTICLE; ASTRONOMY; CHEMISTRY; EQUIPMENT DESIGN; HUMAN; INSTRUMENTATION; METHODOLOGY; MICROCLIMATE; SPACE FLIGHT; WATER SUPPLY; WEIGHTLESSNESS;

AIR CONDITIONING; CARBON DIOXIDE; ECOLOGICAL SYSTEMS, CLOSED; EQUIPMENT DESIGN; HUMANS; LIFE SUPPORT SYSTEMS; MARS; OXYGEN; SPACE FLIGHT; SPACECRAFT; WATER SUPPLY; WEIGHTLESSNESS; ZEOLITES;

EID: 0035263258     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(01)00051-0     Document Type: Conference Paper

References (7)

1. International space station program, subsystem analyses and analytical models
2. Living together in Space: The design and operation of the live support system on the international space station
3. International space station carbon dioxide removal assembly testing
4. Air revitalization system demonstrator design and test results
5. Recent regenerative ECLSS technology developments in Europe
6. ISS oxygen generation design status