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
01.01.2012
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
RELIABILITY BASED DESIGN OPTIMIZATION OF A CUBESAT DE-ORBITING MECHANISM
British Library Conference Proceedings | 2012
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