2007, Volume 9, Issue 7
Strategic Study of CAE >> 2007, Volume 9, Issue 7
Reliability Design and Analysis of Spacecraft Thermal Cont rol/Thermal Management System
School of Aeronautic Science and Technology, Beihang University, Beijing 100083, China
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Abstract
Based on the developing demand of spacecraft thermal control and thermal management, basic design schemes and analysis models for maintaining thermal control/thermal management system's reliability are developed through classifying and reviewing of common spacecraft thermal systems and devices. Examples are given to show the application patterns and methods of the reliability design schemes and analysis models, which provide a fundamental tool for advanced design and analysis for the reliability of spacecraft thermal control and thermal management system.
Keywords
spacecraft ; thermal control ; thermal management ; reliability
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References
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