US Lab IATCS Hardware and Software Integration Development Test

961351

07/01/1996

Event
International Conference On Environmental Systems
Authors Abstract
Content
The International Space Station (ISS) Internal Active Thermal Control System (IATCS) performance has been studied during the Hardware/Software Integration (HSI) Brassboard Development Testing. The ITCS Brassboard Development Test was built to verify the flight Thermal Control System performance and control. This paper describes the key results obtained with the flight like Pump Package Assembly, System Flow Control Assembly, Loop Cross-over Assembly, and Three Way Mixing Valve embedded in development hardware driven by flight software operated on a Functional Equivalent Unit Multiplexer-Demultiplexer (MDM).
Meta TagsDetails
DOI
https://doi.org/10.4271/961351
Pages
11
Citation
Sleiman, A., and Rogers, S., "US Lab IATCS Hardware and Software Integration Development Test," SAE Technical Paper 961351, 1996, https://doi.org/10.4271/961351.
Additional Details
Publisher
Published
Jul 1, 1996
Product Code
961351
Content Type
Technical Paper
Language
English