The space shuttle orbiter atmospheric revitalization subsystem provides thermal and contaminant control as well as total- and oxygen partial-pressure control of the environment within the orbiter crew cabin. Challenges that occurred during the development of this subsystem for the space shuttle orbiter are described. The design of the rotating hardware elements of the system (pumps, fans, etc.) required significant development to meet the requirements of long service life, maintainability, and high cycle-fatigue life. As a result, a stringent development program, particularly in the areas of bearing life and heat dissipation, was required. Another area requiring significant development was cabin humidity control and condensate collection.
Challenges in the development of the orbiter atmosphere revitalization subsystem
1985-01-01
Conference paper
No indication
English
Shuttle Orbiter Atmospheric Revitalization Pressure Control Subsystem
SAE Technical Papers | 1982
|International Space Station Integrated Atmosphere Revitalization Subsystem Testing
SAE Technical Papers | 1996
|Orbiter thermal control subsystem development
NTRS | 1978
|Controls Design for the Space Station Freedom Atmosphere Revitalization Subsystem
SAE Technical Papers | 1993
|