Spacelab ECLS Follow-On-Development

820848

02/01/1982

Event
Intersociety Conference on Environmental Systems
Authors Abstract
Content
With Spacelab approaching its operational stage, ESA has initiated the Follow-On Development Programme. The future evolution of Spacelab elements in a continued U.S./European cooperation is obviously linked to the U.S. STS evolution and leads from the sortie mode improvements (Initial Step) towards pallet systems and module applications in unmanned and manned space platforms (Medium and Far Term Alternatives). The main design driver for the life support system in the Initial Step is the extended mission duration (20 days). This improvement will make Spacelab compatible with the Shuttle EDO.
The Medium and Far Term Alternatives are oriented around the Science and Applications Manned Space Platform and the Space Operations Center considering Spacelab module applications for future manned space platforms. The preliminary definition of the design on subsystem level for regenerative life support systems with various degree of closure has been completed in early 1982.
Meta TagsDetails
DOI
https://doi.org/10.4271/820848
Pages
12
Citation
Skoog, A., "Spacelab ECLS Follow-On-Development," SAE Technical Paper 820848, 1982, https://doi.org/10.4271/820848.
Additional Details
Publisher
Published
Feb 1, 1982
Product Code
820848
Content Type
Technical Paper
Language
English