Simulation and Analysis of Vacuum Swing Adsorption Units for Spacesuit Carbon Dioxide and Humidity Control-Reference-Cited by-同舟云学术

Simulation and Analysis of Vacuum Swing Adsorption Units for Spacesuit Carbon Dioxide and Humidity Control

Published:2011-07-17 Issue: Volume: Page:
ISSN:
Container-title:41st International Conference on Environmental Systems
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Author:

Swickrath Michael¹,Anderson Molly¹,McMillin Summer²,Broerman Craig³

Affiliation:

1. NASA Johnson Space Center

2. Jacobs

3. Hamilton Sundstrand

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-5243

Reference16 articles.

1. Development of Pressure Swing Adsorption Technology for Spacesuit Carbon Dioxide and Humidity Removal

2. 2Hanford, A. and Pinckney, J. “Summary of Testing to Date for the Rapid Cycle Amine Test Articles,” Tech. Rep. ESCG-4470-09-TEAN-DOC-0105-A, Engineering and Science Contract Group, Houston, TX, August 2009.

3. 3McMillin, S. “Engineering Science Contract Group Test Article 2 Rapid Cycle Amine (RCA) Carbon Dioxide And Humidity Removal System Test Report,” Tech. Rep. ESCG-4245-10-EVAHS-DOC-0084, Engineering and Science Contract Group, Houston, TX, September 2010.

4. 4McMillin, S. “Hamilton Sundstrand Rapid Cycle Amine (RCA) Carbon Dioxide and Humidity Removal System Test Report,” Tech. Rep. ESCG-4245-10-EVAHS-DOC-0006, Engineering and Science Contract Group, Houston, TX, May 2010.

5. 5Swickrath, M. “Hamilton Sundstrand Rapid Cycle Amine (RCA) Carbon Dioxide and Humidity Removal System Analysis Report,” Tech. Rep. ESCG-4470-10-TEAN-DOC-0077, Engineering and Science Contract Group, Houston, TX, June 2010.

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