Integration of Thermal and Environmental Control Systems During Space Station Freedom Early Assembly Phase

Paper #:
  • 921259

Published:
  • 1992-07-01
Citation:
Di Pietro, D. and Tandler, J., "Integration of Thermal and Environmental Control Systems During Space Station Freedom Early Assembly Phase," SAE Technical Paper 921259, 1992, https://doi.org/10.4271/921259.
Pages:
16
Abstract:
An overview of Space Station Freedom Thermal Control System (TCS) and Environmental Control and Life Support System (ECLSS) integration is presented for Stages 2-6. Particular attention is given to issues associated with integrating five distinct, functioning spacecraft with hardware not specifically designed for intermediate stages. Areas specifically addressed include integrated ECLSS temperature and humidity control performance, thermal load balancing, performance and verification requirements, interface verification procedures, TCS activation sequence, resource allocation and Space Shuttle integration.
Access
Now
SAE MOBILUS Subscriber? You may already have access.
Buy
Select
Price
List
Download
$27.00
Mail
$27.00
Members save up to 40% off list price.
Share
HTML for Linking to Page
Page URL

Related Items

Standard
2012-03-20
Training / Education
2018-04-25
Book
2012-11-01
Book
2014-01-01
Standard
2012-03-20
Standard
2012-03-20
Training / Education
2018-03-07
Standard
2012-03-20
Standard
2012-03-20
Standard
2012-03-20
Technical Paper / Journal Article
2004-07-19