1994-06-01

Molecular Sieve CO 2 Removal Systems for Future Missions: Test Results and Alternative Designs 941396

Reversible adsorption on zeolite molecular sieve material allows selective removal of carbon dioxide (CO2) from spacecraft air without the use of expendables. The four-bed molecular sieve (4BMS) CO2 removal subsystem chosen for use on space station is based on proven Skylab technology and provides continuous CO2 removal from the cabin atmosphere and concentration for further processing downstream or venting overboard.
A 4BMS subsystem has also been chosen to remove CO2 from air in the Systems Integration Research Facility (SIRF) at NASA/Johnson Space Center (JSC). After installation in the SIRF in 1992, the subsystem underwent extensive testing in which cycle time, process air flow rate, and process air inlet CO2 composition were varied. In order to obtain performance data required for integration, the subsystem was operated under both nominal and off-nominal conditions. Results of this testing are presented.
For future missions, alternative subsystem designs and operational modes for a molecular sieve-based CO2 removal subsystem may be more desirable than the baseline 4BMS subsystem, depending on mission drivers. In addition, development of new adsorbent materials may result in significantly lower power and weight penalties for a molecular sieve CO2 removal system. Alternative designs to the existing 4BMS configuration, which utilize existing hardware components and were considered during the space station redesign effort, are presented and discussed.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Determination of On-Orbit Cabin Air Loss from the International Space Station (ISS)

2004-01-2597

View Details

TECHNICAL PAPER

Development of a Rotary Separator Accumulator for Use on the International Space Station

2002-01-2360

View Details

TECHNICAL PAPER

Development of an Electrostatic Suspension Reaction Sphere

640203

View Details

X