Reliability Based Design Optimization of a CubeSat De-Orbiting Mechanism
12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
2012-01-01
Conference paper
Electronic Resource
English
RELIABILITY BASED DESIGN OPTIMIZATION OF A CUBESAT DE-ORBITING MECHANISM
British Library Conference Proceedings | 2012
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