Spacelab ECLS Current Status

820884

2/1/1982

Authors
Abstract
Content
The Spacelab Environmental Control/Life Support Subsystem (ECLS) provides an earth-like “shirtsleeve” environment in the Spacelab cabin compatible with the atmosphere of the Orbiter crew compartment. This paper describes the major ECLS functions with particular respect to the current Flight Unit hardware status. It also includes recent design modifications, improvements, and adaptations resulting from Spacelab qualification and integration. ECLS potential atmospheric interaction with the Orbiter ECS is presented as well. In the course of extensive performance testing, the Spacelab ECLS design has proven its capability to meet specified performance and to provide adequate operational support.
Meta TagsDetails
DOI
https://doi.org/10.4271/820884
Pages
12
Citation
Lautenbach, P., "Spacelab ECLS Current Status," SAE Technical Paper 820884, 1982, https://doi.org/10.4271/820884.
Additional Details
Publisher
Published
2/1/1982
Product Code
820884
Content Type
Technical Paper
Language
English