BIOSATELLITE Environmental Control and Life Support System Design

670839

02/01/1967

Event
Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
This paper presents the environmental control and life-support system design for the 21 and 30 day mission NASA Biosatellite program. A two-loop system is described which provides temperature control for the fuel cell power source, cryogenic gases, water and urine storage, and the gas management system. The latter provides control of the gaseous environment in the recovery capsule. It controls temperature, relative humidity, recirculation and filtration of the atmosphere, buildup of toxic and/or nontoxic gases and odors, and partial and total pressure of the nitrogen/oxygen atmosphere.
Comparison of experimental results with analytical predictions are presented. Extensive thermal vacuum system testing was performed to verify design predictions; good agreement with analysis was achieved.
Meta TagsDetails
DOI
https://doi.org/10.4271/670839
Pages
13
Citation
Ebersole, R., Pochettino, L., and Kugler, W., "BIOSATELLITE Environmental Control and Life Support System Design," SAE Technical Paper 670839, 1967, https://doi.org/10.4271/670839.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670839
Content Type
Technical Paper
Language
English