Abstract
The Cryogenic Systems Integration Model (CSIM) is a Microsoft Windows® 95 based software tool for the simulation and analysis of spacecraft cryogenic mechanical refrigeration thermal control systems. Previous experience has shown that cryogenic systems exhibit large analytical uncertainties. Historically, cryogenic thermal integration has been critical and often inadequately considered during the preliminary design phase resulting in significant revisions and system penalties. CSIM development was initiated in response to the need for an efficient method for the preliminary design and parametric analysis of spacecraft cryogenic mechanical refrigeration systems.
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