The Spacelab (SL-1) thermal/Environmental Control Systems (ECS) are discussed. Preflight analyses and flight data are compared in order to validate payload to Spacelab interfaces as well as corroborate modeling/analysis techniques. In doing so, a brief description of the Spacelab 1 payload configuration and the interactive Spacelab thermal/ECS systems are given. In particular, these interfaces address equipment cooling air, thermal and fluid conditions, humidity levels, both freon and water loop temperatures and load states, as well as passive radiant environment interfaces.
Flight Evaluation of Spacelab 1 Payload Thermal/ECS Interfaces
Sae Technical Papers
Intersociety Conference on Environmental Systems ; 1984
1984-07-01
Conference paper
English
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